SlideShare ist ein Scribd-Unternehmen logo
1 von 245
PHYSICS
 MODULE 2




     www.part66.blogspot.com
Basic SI Units

              Length     (L)       Metre (m)
              Mass       (m)       Kilogram(kg)
              Time        (t)      Second (s)



                       Derived SI Units

 Area        (A)                 Square Metre      (m2)
 Volume      (V)                 Cubic Metre       (m3)
Density     (ρ)                 Kg / Cubic Metre (kg/m3)
 Velocity    (V)                 Metre per second (m/s)



       Force     (F)                      Newton    (N)
       Pressure(p)                        Pascal   (Pa)
        Energy (E)                         Joule     (J)
        Work      (W)                      Joule     (J)
       Power (P)                          Watt      (w)
       Frequency(f)                       Hertz    (Hz)
matter
• Matter - anything that occupies
  space.
      - consists of atoms and molecules.

• Atom - smallest particle in an element   that
  has the properties of the
        element.

• Molecules - the combination of two or
  more atoms.
NATURE OF MATTER

• Nucleus - each carrying a positive charge are called protons.
In addition to the protons the nucleus usually contains electrically neutral particles
called neutrons. Neutrons have the same mass as protons whereas electrons are very
much smaller.

 • Neutron - simply adds to the weight of the nucleus.
                - has no charge.
 • Proton - positively charged.
                - has mass same as the neutrons.


      • Electron - orbits define the size or volume occupied by the atom
                - negatively charged.
                - total number of negatively charged electrons matches
         number of positively charged protons.
• The sub-atomic components of atoms.

    Particles     Relative       Electrical             Comments
                   Mass           Charge
    Neutron          1           0 ( zero )           In the nucleus
    Proton           1         +1 ( positive )        In the nucleus
    Electron      1 / 1850     -1 ( negative )   Arranged in energy levels
                                                   or shells around the
                                                         nucleus
• Atomic Number – no. of protons in the atom’s nucleus.
      eg. Hydrogen has 1 proton – atomic no. is 1.
          Carbon has 6 protons – atomic no. is 6.

• Mass Number – total no. of protons and neutrons in nucleus.
      eg. Lithium has 3 protons & 4 neutrons – mass no. 7
Relative Atomic Mass

The mass of atom in relation to the mass of a reference atom.

Element chosen on which to relate mass of all atoms is Carbon.

Eg.     Carbon (12) - 6 protons + 6 neutrons
        Hydrogen - 1 proton + 0 neutron = mass no. 1

*so relative atomic mass for Hydrogen is one twelfth of Carbon.
Isotopes
•   are atoms that have same atomic number but different mass numbers.
•   Atom gains / loses one or more neutrons from nucleus will become
    ISOTOPES.




•   Are present in most elements and may also be man made.
• From left to right across a period =
  protons/electrons count increases by one.
• Atomic number = increases from left to
  right.
• Group
1. Vertical column
2. Elements have same number of outer shell
   / valency electrons.

Noble gases - group 8.
Transition metals - middle of the table.
Pure metals - group 1, except Hydrogen.
CHEMICAL COMPOUNDS
• Atoms bond together to form a molecule.

                                     Molecules



       Monatomic Molecule                            Chemical Compounds


  Consists of single type of atom.               Made up of two or more atoms.
Structure of Atoms

•  Electrons are arranged in energy levels and shells around the nucleus and
   with increasing distance from the nucleus .
• Valence electrons :
         - how many electrons an atom has in its outer shell.
         - determines the chemical behavior.
         - The more valence electrons, the more want for the atom to
           get more electrons.
• Valency :
1. bonding capacity of an atom; usually equals the number of unpaired
   electrons in the atoms outermost shell.
2. No. of bonds it can make with a monovalent atom such as Hydrogen.
         Monovalent
         Bivalent
         Trivalent
         Tetravalent
The Molecule
•   A group of two or more similar or dissimilar atoms bonded together .

•   Metallic bonds - metal + metal (eg: Alloy)
                    - do not produce molecules
                    - weakest bonds of all

•   Ionic bonds    - metal + non-metal (eg: sodium chloride)

•   Covalent bonds - non metal + non metal (eg : water)
                    - produce molecules, strongest bond.
Chemical compounds
• Defined as :
‘ A substance made up of different elements that are chemically bonded and
are so united that the whole has properties of its own, which are unlike those
of its constituents.’

• All other molecules made up of two or more atoms are known as Chemical
  compound.
States of matter
• All matter exists in one of three physical states.

• Physical state refers to the condition of a compound and has no

   affect on a compound's chemical structure.

• Solid. A solid has definite mass, volume and shape.

• Liquid. A liquid has definite mass and volume but takes the shape
   of its container.

• Gas. A gas has definite mass but takes the volume and shape of its
   container.

• increase in the temperature will increase the energy of its
   molecules.
Changes between states
• Solid to Liquid – Fusion
i.  Heat energy required to complete process of converting unit
    mass of substance from solid to liquid state without change of
    temperature is called the Latent Heat of Fusion.
• Liquid to Gas – Vaporisation
i.  Heat energy required to vaporise a unit mass of liquid without
    temperature rise is called Latent Heat of Vaporisation.
• Gas to Liquid – Condensation
i.  Heat energy expelled is called the Latent Heat of Condensation.
• Liquid to Solid – Solidification
i.  Loss of molecular energy is the Latent Heat of Solidification.
• Sublimation
i.     Some solid substance when heated do not melt, but form a
       Vapour.

ii.    Solid to vapour, without passing through liquid state.

iii.   Eg. Dry ice



• Evaporation

i.     Liquid change to vapour.

ii.    Some liquid have low boiling point, so easily change from liquid
       to vapour.

iii.   Eg. Methylated spirits.
Mechanics :
          statics ; -
              forces
        centre of gravity
        stress and strain
      properties of matter
pressure and buoyancy in liquids
Newton’s law of motions
First Law of Motion
A body at rest will remain at rest unless given an external force, or a
body which is moving will keep on moving unless given an external
force. ( Inertia )

Second Law of Motion
A force proportional to the rate of change of its velocity is produced
whenever a body ( or mass ) is accelerated.
                 F = ma




Third Law of Motion
For every action, there is an equal and opposite direction.
MECHANICS
STATIC
Forces
• If a Force is applied to a body it will cause that body to move in the
  direction of the applied force.
• force has both magnitude (size) and direction.
• Forces cannot be directly observed, only their effects can be seen.
          Compressive - force applied on an object to squeeze it.
          Tensile - pair of forces try to extend an object.
          Shear - Pair of forces tries to cause one face of material to
           slide relative to an adjacent face.
• Statics is used to describe study of bodies at rest when forces are
  balanced.
• External force – force applied to an object from outside its
  boundaries.
• Internal force – force induced in the object to react against
  externally applied force. ( Reaction )

VECTOR AND SCALAR
• Scalar – just a magnitude, there is no direction associated.
        eg. Time , mass, volume.

• Vector – require both magnitude and direction to be fully defined.
       eg. Force, velocity, acceleration.
Adding Forces
• 2 or more forces act at same line, produce resultant force.
• If at straight line, subtract or addition.




• Forces do not act in a straight line – use the ‘parallelogram law’.
Worked example

Find the resultant of two forces of 4.0 N and 5.0 N acting at an angle of 45
degree to each other.
Using a scale of 1.0 cm = 1.0 N, draw parallelogram ABCD with AB = 5.0 cm,
AC = 4.0 N and angle CAB = 45 degree, see figure 8.
Worked example: three forces acting on a mass.

First resolve each force into its vertical and horizontal components.
MOMENTS AND COUPLES
• If a body free to rotate about some point ;
i.   Applied force will cause rotation
ii.  Force required dependent on how far from hinge force is applied.
iii. Turning effect = magnitude and distance.
         Moment = force x distance.




•   In SI units, Newtons metres = Newton x metres
The Principle of Moments

‘If a body is at rest under the action of several forces, the sum of the
clockwise moments about any axis is equal to the sum of the anti
clockwise moments about the same axis.’

Type 1 – beam balances where arms are of equal length.
Type 2 – lever arrangement can best be seen in design of a
wheelbarrow.
Type 3 – large effort moves through small distance to overcome small
load, which moves through a large distance.
• IN EQUILIBRIUM




• COUPLE – WHEN TWO EQUAL BUT OPPOSITE
  DIRECTION, CAUSES ROTATION
For example, suppose it is necessary to calculate the resultant moment of
a pivot acting on a bell crank lever, refer to diagram below.

         AO        =         100 mm
         OC        =         20 mm
         BC        =         20 mm
WHAT IS
CENTER OF GRAVITY ?
CENTRE OF GRAVITY
• Gravity is a force which is always present and is a pulling force in
   the direction of the center of the earth.



• This force acts on every body through an imaginary point called the
   center of gravity (C of G).



• A point where all the weight of a body appears to be
   concentrated. (total weight can be considered to act through that
   datum position )
(total weight can be considered to act through that datum
position )
•   There must be a datum point, such as where when moment in clockwise
    direction will be balanced by moment in anti-clockwise direction, if given
    the same amount of force.
Stability / balancing
• The lower the C of G, the stable an object is.
• The wider the base, the more stable an object
  is – C of G towards the base.
• The location of the center of gravity in the
   human body varies slightly, depending on
   body shape.

• a male with a muscular upper body and
   small hips, the center of gravity is higher
   than in a female with narrow shoulders
   and wide hips

• in an infant with a large head in relation
   to its body, it is higher than in an adult
• When force applied to
 C of G, the body will not rotate.



• But if the force is applied
  offset of the C of G, the body
  will rotate, or torque will
  produced.
Expressed as an algebraic formula,
         W1 X1 + W2 X2 + W3 X3 = (W1 + W2 + W3) x G

Where G is the position of the centroid, with respect to the datum.
         G=
C of g of an aircraft
Why do we need to know c of g of an
                aircraft ?
•   To ensure the aircraft is safe to fly, the center-of-gravity must fall within
    specified limits established by the manufacturer.

•   C of G range – C of G limits are specified longitudinal (forward and aft) and/or
    lateral (left and right) limits within which the aircraft's center of gravity must
    be located during flight.

•   To evenly load the aircraft – equipments, passengers, baggage, cargo, fuel,
    etc.

•   So that C of G range will not be exceeded – prevent aircraft unstable during
    flight.

•   Also affects C of G in flight – fuel usage, passengers’ movement, etc.
Similar to aircraft, force applied will be acted through the C of G,
resulting in torque.

Aircraft rotate about its C of G.
WHAT IS STRESS ?

AND WHAT IS STRAIN ?
Stress
•   If force is exerted on a body, there will be mechanical pressure acting on
    the body which is called the stress.

•   A body with having twice the size of other body subjected to a force, it will
    be stronger and less likely to fail due to applied the applied force.

•   So, stress is said :

           Stress =



           *units : Newton metre -2 , Nm-2

•   Components will fail due to over-stressed, not over-loaded.
•   Eg. A tennis ball sealed from atmospheric pressure. So, as long as the
    external forces acting on it does not exceed the internal forces, the ball will
    maintain its shape.
•   Forces applied to the body will cause distortion of the body and change to the
    material’s cross-sectional area ;

          eg. Tensile Forces will cause elongation .

              Compressive Force will cause reduction in dimension.

•   Most material have elastic properties ( it will to return to its original shape after
    the force is removed ) - provided forces does not exceed limit of elasticity.
•   There are 5 types of stress in mechanical bodies :
          i. Tension
          ii. Compression
          iii. Torsion
          iv. Bending
          v. Shear
Tension




•   force that tends to pull an object apart

Compression



• resistance to an external force that
tries to push an object together.
Torsion
• Torsional stress is applied to a material when it is twisted.
• Torsion is actually a combination of both tension and compression




Bending
• In flight, the force of lift tries to bend an aircraft's wing upward.
Shear
• combines tension and compression is the shear stress, which tries to slide
   an object apart.
Strain
•   If the outside force is great enough to cause the object to change its
    shape or size, the object is not only under stress, but is also strained.

•   If a length of elastic is pulled, it stretches. If the pull is increases, it
    stretches more; if the pull is reduced, it contracts.



Hooke’s law states that the amount of stretch (elongation) is proportional
to the applied force.
How stress varies with stress when a steel wire is stretched until it breaks.

Hooke’s Law states that, ‘the amount of stretch (elongation) is proportional to
the applied force.’

•   Strain - the degree of distortion then has to be the actual distortion divided
    by the original length (in other words, elongation per unit length).
•   Strain = change in dimension / original dimension ( No units )
*for shearing and torsional stresses, they are expressed as ‘shearing
action’ – when one layer of materials move relative to another in
direction of applied force.

Shear strain – straight motion.
Torsion strain – rotational motion.
Compression strain
Shear strain                          Torsion strain
• when the applied load causes        • form of shear stress resulting
   one 'layer' of material to move        from a twisting action.
   relative to the adjacent layers.




                                      •   Twist will be proportional to the
                                          applied torque.
Shearing Strain
Properties of matter
Diffusion
•   Is the spreading of a substance of its accord.

•   due to molecular action, e.g. a smell, whether pleasant or not, travels
    quickly from its source to your nostrils where it is detected.

•   occurs in liquids and gases but not in solids.
Surface Tension
•   This suggests that the surface of a liquid behaves as if it is covered with an
    elastic skin that is trying to shrink.

•   The surface tension can be reduced if the liquid is ‘contaminated’, adding a
    detergent to the water will cause our needle to sink.

•   In a liquid, the molecules still partially bond together and prevents liquid
    from spreading nag expanding out.
Adhesion

Force of attraction between molecules of
different substances.




Cohesion

Force of attraction between
molecules of same substances.
capillary
•   If a glass tube of small bore is dipped into water , the water rises u the
    tube a few centimetres.

•   The adhesion between the glass and the water exceeds the cohesion of
    the water molecules, the meniscus curves up , and the surface tension
    causes the water to rise.
Mechanical properties of
Strength
               matter
A strong material requires a strong force to break it

Stiffness
A stiff material resists forces which try to change it’s shape or size.

Elasticity
The ability to recover to its original shape and size after the force deforming it has been
reformed.

Ductility
Materials that can be rolled into sheets, drawn into wires or worked into other useful
shapes, without breaking are ductile.

Brittleness
A material that is fragile and breaks easily .
Pressure and buoyancy in
•
               liquid
    The equivalent term associated with fluids is pressure:

          pressure = force / area        or         p = F/A.


•   Pressure is the internal reaction or resistance to that external force.

•   Pascal’s Law : “pressure acts equally and in all directions throughout that fluid.”
pressure can be transmitted to some other point in order to
                  generate another force.
Units of pressure

SI system pressure :
          Pascal = force per unit area ( Nm-2)



Atmospheric pressure :

          Milibars ( mb ) or pounds per square inch ( psi )



Sea level standard atm presssure :

          1013-2 mb or 14.69 psi ( at 0C)
buoyancy
Archimedes’ Principle states that when an object is submerged in a liquid, the object
displaces a volume of liquid equal to its volume and is supported by a force equal to the
weight of the liquid displaced.


                           THE BUOYANCY OF A SUBMERGED BODY =

                     WEIGHT OF DISPLACED LIQUID – WEIGHT OF THE BODY



1. The body will float--if the buoyancy is positive

2.The body will sink--if the buoyancy is negative

3.The body will be stuck--if the buoyancy is neutral
kinetics
Linear motion
• Is the uniform motion in a straight line.
• Motion is the change of position of a body with reference to
  another body.

        eg.      A person sitting in a moving car and passes a
                 building.

                  The person is considered to be at a state of
        rest in reference to the car.

                  The car is considered to be in motion in
        relation to the building.
speed
•   Speed tells us how quickly an object is moving at any given point in time.

•   Scalar quantity – does not take into account the direction of the object
    travelled.

•   Average speed – dividing the distance travelled by the time taken.

          Speed     =         rate of change of displacement or position
                    =



          v         =                   where v represents speed.
Worked example



• An aircraft flies at 80 km/ hr for 15 minutes and at 120 km/hr for a
   further 15 minutes. How far has it travelled and what is the
   average speed ?
velocity

•   Includes direction, distance in straight line and time.

•   Vector quantity – magnitude + distance.

          eg.       An aircraft moves 200miles South West
                    from A to B in one hour.

          *the velocity is 200mph South West.
acceleration
•   Is the rate of change of velocity over time.

•   If the rate of change is constant, acceleration is described as being
    uniform.

•   Acceleration - If the velocity of an object increases over time.

•   Deceleration / retardation – If the velocity decreases over time.

•   If a car is travelling at initial constant velocity ‘u’ and then accelerated with
    uniform acceleration ‘a’ to final velocity ‘v’, therefore :

                      a         =         (v–u)/t
                      v         =         u + at

    *Unit : m / s 2
Equation of linear motion
Equations of linear motion

                    V = u + at
                    s=½(u+v)t
                    s = ut + ½at2
                    v2 = u2 + 2as

Free falling objects
• if a stationary object is released and free falls under attraction of the force
    of gravity, it will accelerate at 9.81 m/s 2
• So the ‘a’ will be 9.81 m/s 2 ,
   but in this case it is given the symbol ‘g’.
• If the object is thrown upwards, its g will be – 9.81m/s2
•   Initial velocity of objects freefalling from rest is zero, so the equations for free fall
    are :


        V                       =          gt

        S                       =          ½ gt2

        V2                      =          (2gs)2
ROTATIONAL MOTION
Circular Motion
• Rotational motion means motion involving curved paths and therefore
    change of direction.
• Only cases of constant acceleration are considered here.
• They are equivalent to those linear equations of motion :
Centripetal Force
•   Continuous force applied to a body moving in circular path to keep it in
    that particular circular path, preventing it from travelling in straight line (
    tangential to circle it is rotating in ) – due to the inertia of the object.

•   Basically a force acting inwards toward the centre of the circle.

•   Is directly proportional to the mass of the object in circular motion.

•   Is inversely proportional to the radius of the circle in which the object
    travels.
•   Force = ma, so we can say that the object has an inwards acceleration
    called Centripetal Acceleration which is ;
           a         =          v2 , so              F           =
                                r
           *where v is linear velocity and r is radius of circular path.
Centrifugal Force
• Is the equal but opposite reaction to the Centripetal Force.
  ( Newton’s 3rd Law )




•   Tensile Force at the other end of the string acts outwards of the circle.
Relationship between Angular and Linear Motion :

Providing that we know the value of the rotating
body’s radius ( r ), we can use the relationship
between the radius and the radian to convert angular
values to linear values and vice versa.

      Linear distance    :    rθ
      Linear velocity    :    rω
      Linear acceleration :   rα
Periodic motion
•   Some masses move from one point to another, then back to the original
    point, and continue to do this repetitively.



•   The time during which the mass moved away from, and then returned to
    its original position is known as the time period, and the motion is known
    as periodic motion.



•   Example : pendulum
Pendulum
•   When the mass then displaced from its rest position, it will accelerate back towards
    its rest position.

•   On reaching it however, it will not stop, because its inertia carries it on to an equal
    but opposite displacement.

•   the time period can be measured from a any position, through to the next time that
    position is reached, with the motion in the original direction.
Cycle –for one complete to and fro movement.
Periodic Time – time taken to complete 1 cycle.
Frequency – the number of cycle occurring in 1 seconds. ( Hertz – HZ )
Amplitude – maximum displacement of a body from its middle or rest position.
•   Periodic time, T can be calculated by ;
          T = 2 √ ( L / g )
    Where ;
          L – length of the pendulum
          g – magnitude of acceleration due to gravity = 9.81 m/s2


    For time period ( T ) and frequency ( f ) ;

          T=1/f                ,          f=1/T
Spring – mass systems


•   If the mass at the spring is displaced and the force is released, the spring
    force will cause the mass to return to its original position.

•   It will behave like pendulum, so it continue to move up and down before it
    stops completely.

•   Springs obey Hooke’s Law.

•   The resulting motion, up and down, resulting in :
Spring Force

         Force ( F )           =           mg    =         kE

         if mg = kE, then the spring constant k = mg
                                                       E
         Also, extension E = mg
                                       k

         Frequency (f) = ( 1 / 2 ) √ ( k/m )

         where;

         F is force.
         m is suspended mass.
         g is the acceleration due to gravity.
         E is the spring extension.
         k is the spring constant.
Simple theory of vibration,
•
             harmonics and resonance. but strict law.
    Analysis of oscillating systems will show that they often obey simple
•   Acceleration is proportional to the displacement from the neutral position, and in the
    opposite sense to the direction of the velocity.
•   Referred to as Simple Harmonic Motion, when acceleration is directed towards fixed
    point in its path and is proportional to its displacement from that point.
Vibration theory

• Vibration Theory is based on the detailed analysis of vibrations and is
  essentially mathematical, relying heavily on trigonometry and calculus,
  involving sinusoidal functions and differential equations.
• Damped vibrations :
 Simple pendulum / spring mass will vibrate at constant frequency and
  amplitude, once it is started.
 But vibrations will die away due to other motions such as friction, air
  resistance, etc.
Resonance


•   When force subjected to force vibration, it will vibrate along with natural
    frequency of the object.



•   If the natural frequency matches the resonant frequency with forced
    vibration causes the amplitude to increase dramatically.



•   Natural frequency tries to damped out the amplitude but cannot damp its
    own natural frequency.



•   So the two amplitudes combine to produce resonance.
Velocity ratio, mechanical
           advantage and efficiency.
•   Machine – utilise some form of motion to convert an applied force into a
    useful work output
•   The input forces is often amplified many times by the machine so that we
    can overcome a heavy load with little effort.
•   Eg ; levers, pulleys, gears, screws.

Velocity ratio

•   Ratio of distance the effort is required to move in comparison with the
    distance the load moves in the same time.


        Velocity Ratio = Distance moved by effort
                        Distance moved by load
Mechanical Advantage
• Describes the ratio of load moved with the effort required to move it.

         Mechanical Advantage = Load
                                   Effort

           *A rusty car jack will have a low mechanical advantage because      much of
the effort would be used to overcome the friction of a      corroded screw thread.

Efficiency
• Describes the ratio of the useful work done by a machine to the total work put into
     it.
           Efficiency = Work Output x 100% or Mechanical Advantage x100%
                          Work Input                     Velocity Ratio
• Expressed as percentage and is always less than 100%.

         *Friction and slippage can detract from efficiency of a machine.
LEVERS
• Used to gain mechanical advantage.
• Most basic form : seesaw that has weight at each end.
 ( weight on one end tends to rotate it clockwise, weight on the other end
tends to rotate it anti-clockwise )

First Class Lever

•   Lever has fulcrum between load and effort.
•   Less effort required to lift the load.
Second Class Lever
• Has fulcrum at one end of the lever and effort is applied to the opposite
   force.




Third Class Lever
• Force is applied between fulcrum and load.
• Used to move the load a greater distance than effort applied.
• Disadvantages : much greater effort required to produce moment.
Pulleys
•   Pulley wheel has circumferential groove to accept a rope.

•   Effort is applied by pulling on a rope.

•   Tension created in the rope and movement are transmitted through
    arrangement to the load.

•   Single fixed pulley is a convenient means of lifting a light load.




•   So, for instance, if one end of the rope is attached to a fixed object, pulling on
    the other end will apply a doubled force to any object attached to the axle.
dynamics
Mass
• Is the quantity of matter that it contains.
• Constant regardless of its location.
• Basic SI unit : kilogram (kg)
• Imperial : pounds (lbs)

Weight
• Force with which gravity attracts a body.
• Varies with distance between body and centre of the earth, so if farther
   than centre of the earth, the less it weighs.
• So, it is said that an object in deep space does not has no weight, but do
   has mass.
• Gravitational acceleration is considered as 9.81m/s2

Force
• Is a vector quantity that has magnitude, direction and a point of
   application.
• Which changes a body’s state of rest or of uniform motion.
Inertia
• Newton’s First Law
• A body at rest will stay at rest unless given an external force, or a moving
    body will continue on moving unless given and external force.
• Is the resistance to movement or changes.

Work
• Work is done when a force move.
            Work done = force x distance moved in the direction of the force.
•   Unit : Newton metre (Nm) or the joule
            1 joule = the work done when a force of 1 Newton is applied through
                        a distance of 1 metre
Power
• The amount of work done in specific time.
       Power = work done            =    force x distance
                    time taken                  time

• Si unit : Watt ( W ) – 1 Joule/ second
• Is the rate of work done when 1 Joule is achieved in one second.
*One horsepower is the equivalent of 746 Watts

Brake Horse Power
• To rate the engine power.
• The engine is made to do work on a device known as dynamometer or ‘brake’ –
   loads the engine output.

Shaft Horse Power
• Measure output shaft of a turboprop engine, since the power produced at shaft
   is what will be delivered to propeller.
Energy
•   Is the capacity to do work.

•   Si unit : Joules

•   Can appear as several form ; mechanical, chemical, heat, electrical, and
    radiation.

•   But only deal with Mechanical Energy, and appears as potential and
    kinetic energy.

•   Energy cannot be created or destroyed, it can only be changed from one
    form to another.

•   Energy will not be converted into 100% work, they will always appear in a
    less useful form such as wasted heat.

•   But it may be converted into 100% energy.
Potential Energy (PE)


•   Energy is possesses by virtue of its position or state.

•   Example : A mass raised to a height above the ground has potential energy
    since its weight is capable of doing work as it descends to the ground
    under the influence of gravity.

          Work = force x distance

*since PE is for mass at elevated position,so distance is the height above
ground.

          Potential Energy = mass x gravity x height

                               = mgh
Kinetic Energy

•   Energy it possesses by virtue of its motion.

•   Arises from the work done on it.


•   When body set in motion by a force doing work it acquires kinetic energy,
    which will work against any forces that try to resist it.


          Kinetic Energy        =         ½ mv2
Conservation of Energy


          “ Whenever energy is converted from one form to another,

                                none of it is lost.”



•   The sum of the energy can always be accounted for in the other forms of
    energy that may have converted into.

•   After an object hits ground on a fall, the energy has converted into heat
    energy and will be dissipated into the air.

•   So a comparison between work out and work in is obviously a measure of
    the system efficiency.

          Efficiency = work output

                        work input

*usually expressed as percentage ( less than 100 % ).
Heat
•   Defined as energy between two bodies because of difference in
    temperature.

•   If two bodies at different temperature, are bought into contact, their
    temperature become equal.

•   Energy that flows from a hot place to a cooler place.

•   Heat energy can be transferred by ; conduction, convection and radiation.
momentum
•   Product of its mass and velocity.

          momentum = mass x velocity

•   SI unit ; kgm/s

Impulse of a force
• If a body was subjected to a sudden blow, shock load or impact, it will be
   possible to measure change in momentum.
• Forces which have the short time duration are called the Impulsive forces.
• Change of momentum due to impulsive force is called the Impulse.
• Impact duration small – impulsive force large.
  Impact duration large – impulsive force small.
Impulse
•   Product of force and time or change in momentum.

•   For example, if we rest the hammer, on top of the head of a nail, neither
    the hammer nor the nail has any momentum.

•   However, if we bring the hammer down from a height and strike the nail
    sharply on its head, both the hammer and nail will move after the impact.
    In a short time they will come to rest with the nail having penetrated
    whatever it is under it.

•   Impulse = change in momentum = mass x change in velocity.

            = force ( N ) x time ( seconds )
CONSERVATION OF MOMENTUM

“When two or more masses act on each
other, the total momentum of the masses
remains constant, provided no external
forces, such as friction, act.”
CONSERVATION OF MOMENTUM

          MOTION                           MOMENTUM

First law                                   First Law
Mass remains at rest or continue to         Mass remains at rest or continue to
move at constant velocity, unless acted     move at constant velocity, unless acted
on by an external force.                    on by an external force.



Second Law                                  Second Law
     F = ma                                 Rate of change of momentum is
                                            proportional to the applied force.



Third Law                                   Third Law
For every action, there is a n equal and    If mass A exerts force on B, then B exerts
opposite reaction.                          an equal but opposite force on A.
Changes in Momentum

        Change of Momentum = final momentum - initial momentum
                          = ( mv)            -        (mu)

            Rate of change of momentum = change in momentum
                                              time taken
                                       = mv–mu
                                                 t
*The rate of change of momentum is proportional to magnitude of force
causing it.


•   When two bodies, one of low mass and the other of high mass, are acted
    upon by the same force for the same time, the low body mass will build up
    higher velocity than the heavy mass.
For example;

At (a) – mass A overtakes mass B.
At (b) – mass B will be accelerated by impulsive force delivered by   mass A,
and mass A will be decelerated by an impulsive force delivered by B   .
At (c) – after the impact, mass A and B will have new velocities Va   and Vb.

Momentum before impact equals to momentum after impact.
Example :



A moving snooker balls, each ball has its own momentum before collision. After collision,
the sum of the two balls’ momentum will be the same as the sum prior to the collision
even though their velocities may have changed.


sum of momentums of balls =            sum of momentum after impact
        prior to impact

            mu1 + mu2                  =                   mv1 + mv2
Moment of inertia

•   considers the effect of mass on bodies whose moment is rotational.

•   Moment of inertia is a function of mass and radius.




•   Consider the two cylinders, of equal mass, but different dimensions,
    capable of being rotated.

•   The LH cylinder is easier to rotate than RH cylinder.
GYROSCOPES


•   is a rotor having freedom of motion in one or more planes at right angles
    to the plane of rotation.

•   used in several of an aircraft’s instruments, which are vital to the safety of
    the aircraft in bad weather.

•   For example wheels, engines, propellers, electric motors and many other
    components must run with perfect smoothness.
•   With the rotor spinning, the gyroscope will possess two fundamental
    properties:

          Gyroscopic rigidity or inertia

          Gyroscopic precession
Gyroscopic rigidity
•   maintains the axis of rotation constant in space.

•   if a gyroscope is spinning in free space and is not acted upon by any outside
    influence or force, it will remain fixed in one position.

•   The degree to which the rotor offers resistance depends on 3 things :

         Mass of the rotor – greater the mass, greater resistance to change in
         direction of plane of rotation.

      Angular speed of the rotor – higher the speed, greater the resistance.

      Radius of gyration of the rotor – bigger the radius, greater the rigidity.
Gyroscopic Precession
•   angular change of direction of the plane of rotation of a gyroscope, as a
    result of an external force.

•   The rate of this change can be used to give indications such as the turning
    rate of an aircraft.
I.     The rotor will rotate about axis AA.
II.    Apply a force so that it acts on the rim of the rotor at 900.
III.   Move this force around the rim of the rotor so that it moves through 900
       and in the same direction as the rotor spins.
IV.    Precession will move the rotor in the direction that will result in the axes
       of applied force and of rotation coinciding.
V.     For a constant gyroscopic speed, the rate of precession is proportional to
       the applied force.
VI.    The opposite also applies, so for a given force the rate of precession is
       inversely proportional to rotor speed.
Attitude indicator.
Determining Precession Direction

•   If a mass is mounted on a rotating shaft, and the centroid is offset from
    the axis of rotation, mass will exert centrifugal force on the shaft.
•   Even if the eccentricity is small, force may be considerable at high speed.




•   So, it will cause the shaft to bend.
•   If large stresses produced, will cause damage to bearing.
•   Addition by vibrations from supports and surroundings will cause
    undesirable effect.
•   Some eccentricity is due to manufacturing imperfections or design, so it is
    unavoidable.
•   Balancing is needed to eliminate effect of centrifugal force.
•   Eg ; weights put on car wheels to balance them, make it easier to drive at
    high speed.
Friction


•   Force that resists any sliding movement between two contacting surfaces.

•   Can be taken as advantage, for brakes on vehicle to try to walk on smooth
    surface.

•   Frictional force depends on nature between two surfaces.

•   Acts in any directions but always acts in opposing motion.
•   angle of the plane (θ) is increased, the body remains stationary, until at
    some particular value of θ, it begins to move down the plane.
•   At this maximum value, the force opposing motion
           Fmax = mg sin θ ,
•   and the normal reaction between the body and the plane
           R = mg cos θ.
           F/ R = mg sin θ / mg cos θ = tan θ
•   ratio F/R (tan θ) is termed the Coefficient of Friction ( μ ) - < 1.
           μ         =          F         =         tan θ
                                R
Coefficient of Static Friction



•   Static friction is friction between two solid objects that are not moving
    relative to each other.

•   The static friction force must be overcome by an applied force before an
    object can move.

•   The maximum possible friction force between two surfaces before sliding
    begins is the product of the coefficient of static friction.

•   sometimes referred to as limiting friction.
•   Coefficient of Static Friction (μ) =   Friction Force ( F )
                                                     Normal Reaction ( N )
•   Frictional Force , F = μN
Coefficient of Dynamic Friction



•   Dynamic friction is when two objects are moving relative to each other
    and rub together (like a sled on the ground).

•   The amount of force required to keep the object moving is called the
    coefficient of dynamic friction.

•   usually less than the coefficient of static friction for the same materials
There are several types of friction:

•   Dry friction resists relative lateral motion of two solid surfaces in contact.
    Dry friction is subdivided into static friction between non-moving surfaces,
    and kinetic friction between moving surfaces.

•   Fluid friction describes the friction between layers within a viscous fluid
    that are moving relative to each other.

•   Lubricated friction is a case of fluid friction where a fluid separates two
    solid surfaces.

•   Skin friction is a component of drag, the force resisting the motion of a
    solid body through a fluid.

•   Internal friction is the force resisting motion between the elements
    making up a solid material while it undergoes deformation.
Fluid dynamics
•   Fluid – term used for liquid and gases.

Specific gravity and density

•   Density – mass per unit volume.
•   Varies with :

          Temperature ( for solids and liquid )
          Temperature and pressure ( gas )

            Density ( ρ ) = mass
                              volume
•   Eg : liquid that fills a certain container has a mass of 756 kg. The container
    is 1.6 m long, 1.0 m wide and 0.75 of a metre deep. The liquid density
    should be ?
                       ρ          =         756       =         630kgm-3
                                             1.2
•   Standard conditions for the measurement of gas density is established at
    00C and a pressure of 1013.25 milli-bars

    (Standard atmospheric pressure).



•   Temperature change will not change the mass of the substance, but as
    temperature change, the substance tend to expand or contract, altering
    the volume.
Relative Density
•   It is necessary to compare density of one substance with the other to
    achieve a standard which all other substance can be compared.



•   For solid and liquid, compare with water at 40C.



•   For gas, compare with air.

          Relative Density = mass of any volume of a substance

                                  mass of equal volume of water / air



•   Eg ; if a hydraulic fluid has relative density of 0.8, then 1L of the liquid
    wieghs 0.8 times as much as 1L of water.
Hydrometer
•   Used to measure the relative density of liquids.

•   Glass float contained within cylindrical glass body.

•   Weight at the bottom, scale at the top.

•   When liquid drawn into the body, float displays relative density on
    graduated scale.

•   Immersion in pure water will give out reading of 1.000.

•   App. in aviation : to measure battery electrolyte and fuel.
Viscosity

•   Measure of the resistance of a fluid which is being deformed by either
    shear stress or tensile stress.
•   Also known as "thickness" or "internal friction“.
•   Eg : water has ‘thin’ velocity, while honey has ‘thick’ velocity.
•   so there is friction between two liquid surfaces even when they consist of
    the same liquid.
•   This internal friction opposes the motion of one layer over another and,
    when it is great, it makes the flow of the liquid very slow.
•   Viscosity of a liquid rapidly decreases as its temperature rises.
•   Viscosity of different liquids can be compared in different ways.

•   Eg ; if we allow fluids of different viscosity run out of container, the
    higher the viscosity, the longer time taken to empty the container.

•   It is important to know about viscosity as aircraft uses fluids such as oil
    in the engine for lubrication.
Fluid Resistance



Skin friction
• Resistance present on a thin, flat plate which is edgewise on to a fluid flow.
• Near the surface, the fluid is slowed up due to roughness of the skin, and
    fluid can also be considered as stationary at the surface.
• Effected by skin smoothness.
• The rougher the skin, the higher the friction.
Eddies or turbulent airflow
• swirling of a fluid and the reverse current created when the fluid flows past
   an obstacle.
• The moving fluid creates a space devoid of downstream-flowing fluid on the
   downstream side of the object.
• Eg. If you put plate at right angles to flow, turbulence will be created behind
   the plate and a very high resistance .
Effect of streamlining
• flowing steadily over a smooth surface, narrow layers of it follow smooth
    paths that are known as streamlines.
• This smooth flow is also known as laminar flow.
• If laminar flow encounter obstructions, the streamline will break and
    become irregular or turbulent.



If fluid flows slowly along pipe,
 the flow is streamline.



If flow is very fast and exceeds
a certain critical speed,
the flow will become turbulent.
The Compressibility of Fluids


•   All fluids are compressible, so that their density will change with pressure.

•   Fluid ;

              i. assume as incompressible – provided under steady flow
              conditions, and changes of density small.

•   Gases ;

              i. easily compressed – except when changes of pressure and
              density are small.
Static and Dynamic Pressure




•   Pressure acting on x x1 is due to the weight of the fluid acting downwards.
•   W = mg ( g = gravitational force )
  mass = volume x density
          = height x cross-sectional area x density
          = hAρ
so, downwards force = h . ρ . g . A acting on A
and pressure will be = h ρ g . A
                               A
                         =hρg
Static pressure



•   Act depth h, within a stationary fluid of density ρ.

•   Reduces density accompanied by reduced pressure.



Dynamic pressure



•   Eg, moving air is essential in flight.

•   Dynamic presssure = ½ ρv2 where ρ = density, v = velocity.
Worked example

What is the pressure at 10.5 m deep of liquid in a pool having the density of
2.5kg/m3 ?



What is the depth of an object from the surface if pressure exerted on it is
100psi in a 5.3kg/m3 liquid ?
Bernoulli’s Theorem
• a principle that explains the relationship between potential and kinetic
   energy in a fluid.
• In a fluid the potential energy is that caused by the pressure of the fluid,
   while the kinetic energy is that caused by the fluid’s movement.
• As a fluid enters a venturi tube, it is travelling at a known velocity and
   pressure.
• When the fluid enters the restriction it must speed up, or increase its
   kinetic energy. However, when the kinetic energy increases, the potential
   energy decreases and therefore the pressure decreases.
thermodynamics
Laws Of Thermodynamics


First Law
Energy cannot be created or destroyed. It can only be converted from one to
another. When the energy converts from one form into other forms the total
quantity of energy remains the same.


Second Law
Heat can only transfer from a high temperature region to a lower temperature
region. It cannot naturally transfer the other way.


Third Law
The transfer of energy from matter becomes increasingly difficult as its
temperature approaches absolute zero. It is considered impossible at absolute
zero.
Temperature
• Heat is a form of energy that causes molecular agitation within a material.
• is a measure of the kinetic energy of molecules.
• Temperature scale;
         Freezing – 00C
         Boiling – 1000C
• Farenheit Scale - when you increased the temperature of a gas by one
   degree Celsius, it expands by 1/273 of its original volume.
• So if the temperature was decreased to 273 degrees below zero, the
   volume of the gas would also decrease to zero, and there would be no
   more molecular activity – absolute zero.
• On the Celsius scale absolute zero is - 2730C. On the Fahrenheit scale it is
   – 4600F.
• Conversion ;
    – °C x 9/5 + 32 = °F ( from Deg. Centigrade to Farenheit )
    – (°F - 32) x 5/9 = °C ( from Farenheit to Deg. Centigrade )
Heat
• is the exchange of thermal energy from a hot body to a cold body.
• When a hot body and a cold body have contact, heat will flow from the
    hot body to the cold body until they both reach thermal equilibrium (they
    are at the same temperature).
• For example ;
When an aircraft’s brakes are applied, the kinetic energy of the moving
aircraft is changed into heat energy by the rubbing action of the brake friction
material against the brake discs.
• SI system :
            Joule (J)
            British thermal unit (Btu)
            calorie (cal)

                         Heat & Work Conversion Factors
                1J                    0.2388 cal
                1 cal                 4.1868 J
                1 Btu                 1055 J
                1J                    0.000 947 Btu
                1 Btu                 0.252 cal
                1 cal                 3.968
Heat Capacity


•   specific heat - amount of heat per unit mass required to raise the
    temperature by one degree Celsius.

•   Relationship between heat and temperature change :

          Q = cmΔT



          Q is the heat added in 0C

          C the specific heat capacity in J / kg0C

          M is the mass in kg

          ΔT is Tfinal – Tinitial in 0C
•   Different materials require differing amounts of heat energy to change
    their temperature.

•   The heat energy required to change the temperature of 1 kg of material by
    1 K is known as the specific heat capacity (c) of the material.

•   Due to the high specific heat of water, oceans and large lakes serve as
    temperature stabilisers.

•   Land surfaces have a much lower specific heat, and the temperature can
    vary significantly throughout the day.
Heat Transfer



•   three methods by which heat is transferred from one location to another
    or from one substance to another, which are :

          conduction

          convection

          radiation
Conduction

•   When body having high heat energy in contact with body having low heat
    energy.

•   Eg; When hot object in contact with cold object, energy of molecules from
    hot object will be transferred to molecules of cold object until they have
    the same amount of energy ( stabilize ).

•   Various metals have different rates of conduction.

•   Liquids are poor conductors of heat in comparison with metals.

•   .Gases are even worse conductors of heat than liquids.

•   Insulators are materials that reduce or prevent heat conduction.
Convection



•   process by which heat is transferred by the movement of a heated fluid.

•   Transfer of heat by convection is often hastened by the use of a ventilating
    fan to move the air surrounding a hot object.

•   Eg ; when heat is absorbed by a free-moving fluid, the fluid closest to the
    heat source expands and its density decreases.
Radiation

•   is the only form of energy transfer that does not require the presence of
    matter.

•   refers to the continual emission of energy from the surface of all bodies.

•   This energy is known as radiant energy of which sunlight is a form.

•   This is why you feel warm standing in front of a window whilst it is very

    cold outside   .
Expansion and Contraction

•   All materials expand and contract with a change in temperature.

            gases which expand the greatest amount .

            Solids and liquids expand much less than gases
Volumetric Expansion

•   Expansion – considered as change in length, change in area or change in
    volume.
•   Different materials expand at different rates.

Expansion of Solids
• Expansion is proportional to the increase in temperature to the original
   dimension and depends on the actual material used.

          L2 - L1   =         L1 (θ2 - θ1)α

          L2 and L1 are final and initial lengths,
          θ2 and θ1 are final and initial temperatures
          α is a material constant (coefficient of linear expansion).
Expansion of Fluids


•   Fluids expand more than solids.

•   For gases, as volume and temperature changes are usually accompanied
    by pressure changes.
The law of Thermodynamics

•   Thermodynamics is the study of the way that one does work with heat.




•   Energy conservation limits the amount of work we can get out of a certain
    amount of heat.
first law of thermodynamics
• States that energy is conserved.
• The change in internal energy of a system is equal to the heat added to
     the system minus the work done by the system.

          ΔU = Q – W

          (Δ is the mathematical symbol for a change in a quantity)
                      ΔU          is the change in internal energy,
                      Q           is the heat added to the system
                       W          is the work done by the system.
•   ΔQ is positive if it is put into the system, negative if it is taken out of the
    system.
•   ΔW is positive if the system does work on its surroundings and is negative
    if work is done on the system.
•   The internal energy is the sum of the kinetic and potential energy of the
    atom and molecules that make up the system.
second law of thermodynamics
•   general principle which places constraints upon the direction of heat
    transfer and the attainable efficiencies of heat engines.

•   States that heat transfer will occur naturally of its own accord down the
    temperature gradient.

•   Heat will naturally flow from a hot region to a cool region but not the
    other way around.
•   the basic sense of the principle :



          Heat will not flow spontaneously from a cold object to a hot
          object.



          You cannot create a heat engine which extracts heat and    converts
it all to useful work.



          There is a thermal bottleneck which constrains devices     which
convert stored energy to heat and then use the heat        to accomplish
work.
gases
•   Ideal gas - one in which all collisions between atoms or molecules are
    perfectly elastic and in which there are no intermolecular attractive forces.

•   a collection of perfectly hard spheres which collide but which otherwise
    do not interact with each other.

•   all the internal energy is in the form of kinetic energy and any change in
    internal energy is accompanied by a change in temperature.
From the Ideal Gas Law ;

                           =
Boyle’s Law

If temperature is constant ;

                     P1V1      =   P2V2


Charles’ Law

If pressure is constant ;

                               =
Isothermal and Adiabatic Processes

Isothermal process - in which the temperature in a system remains constant.
Adiabatic process - one where no heat is added to, or taken away from the
system.

Heat engine

•   heat engine is a system that performs the conversion of heat or thermal
    energy to mechanical work.
Heat Engine Processes




•   a useful process is the adiabatic process where no heat enters or leaves
    the system.
•   The first law of thermodynamics with Q=0, i.e. heat = zero shows that all
    the change in internal energy is in the form of work done.
•   internal energy is proportional to temperature, there is no change in the
    internal energy of the gas during an isothermal process.
•   All the heat added to the system is used to do work.
Engine Cycle
Carnot Cycle
• consisting of two isothermal processes and two adiabatic processes.
• can be thought of as the most efficient heat engine cycle allowed by
   physical laws.
• the Carnot efficiency sets the limiting value on the fraction of the heat
   which can be so used.
• In order to approach the Carnot efficiency, the processes involved in the
   heat engine cycle must be reversible and involve no change in energy
   available to do work.
• This means that the Carnot cycle is an idealisation, since no real engine
   processes are reversible and all real physical processes involve some
   increase in energy available to do work .
Heat Flow to Hotter Region




•   internal energy will not spontaneously flow from a hot region to a cold
    region.
•   But if external force is given, heat can flow from cold region to hot region.
•   Usually this is done with the aid of a phase change, i.e., a refrigerant liquid
    is forced to evaporate and extract energy from the cold area. . Then it is
    compressed and forced to condense in the hot area, dumping its heat of
    vaporisation into the hot area.
Refrigerator
Heat Pump
Optics ( light )
Speed Of Light



•   is one form of transmission of Electro-magnetic energy.

•   travels at high speed (about 3 x 108 metres per second) and in straight
    lines.

•   Can be ‘bent’ or reflected.
Laws Of Reflection and Refraction

Reflection
• Light can also be reflected.
• Observation and measurement will show that ;
          a. the incident and reflected rays lie in the same plane.
          b. the angle of incidence equals the angle of reflection.
Plain and Curved Mirrors

•   When you look in a mirror, you see a reflection, usually termed an image.
•   For example, if an object is viewed from two different angle, the reflected
    rays :
     – appear to come from which corresponds to the image.
     – lies on the same normal to the mirror as the object.
     – appears the same distance behind the mirror as the object is in front.
     – Appears as the same size.
•   For mirror that is not plain, it may be curved, spherical and parabolic.
•   Incidence equals reflection - still holds, but the curved surface allows the
    rays to be focused or dispersed.




                                 FP is known as the focal length.
                                 Note the rays actually pass through F, and a
                                 real image can be formed.




                                 FP is still the focal length, but the image is
                                 virtual.
•   The size of the image depends on the position of the object.
•   image may be smaller or larger.




•   If the object is near to the mirror, the image will be far and larger from the
    mirror but in opposite plane.
•   If the object is far from the mirror, the image will be nearer and small,
    between the position of object and mirror in opposite plane.
           magnification = image height
                                object height

•   For spherical mirror, magnification = image distance
                                              object distance
•   Concave mirrors (e.g. shaving mirrors) give a magnified, erect (right way
    up) image, if viewed from close-to.



•   Convex mirrors (e.g. driving mirrors) give a smaller, erect image, but with a
    wide field of view.



•   Parabolic reflectors can focus a wide parallel beam. By placing the bulb at
    the focus, they can produce a strong beam of light. (Conversely, they can
    focus microwave signals when used as an aerial).
Refraction




•   A submerged object is often seen at reduced depth.
•   This is because the ray has been ‘bent’ at the water / air boundary.
Refraction Index




•   Since the angle of incidence and refraction is not the same ;
          sine i = μ ( a constant )
          sine r
•   depends on the 2 mediums involved.
          μ = speed of light in medium 1
              speed of light in medium 2
Ray (1) has been refracted across the
boundary, but ray (2) has been internally
reflected at the boundary.




critical angle of incidence when the ray in the
denser medium does not emerge, but travels
along the boundary.



•   sine C = 1 / μ exists

•   Refraction is the basic principle which
    explains the workings of prisms and lenses.
Total Internal Refraction
• Refraction at a denser medium, a beam of light is bent towards the normal
    and, vice versa.




•   APB – ray reflected away.
•   AP’D – angle of incidence increased, angle of refraction becomes
    900 .
•   AP”C – Angle of incidence further increased , angle of refraction is >900 ,
    remaining in the boundary.

•   Total internal refraction – where none of lights passing through the
    boundary.
Convex and Concave Lenses
•   The light rays then meet the surface of the lens at an angle to the normal,
    and are then refracted.




•   Images can be real or virtual, erect or inverted, and larger or smaller.

•   The nature of the image will depend on the type of lens, and the position
    of the object in relation to the focal length of the lens, (the focal length is
    a function of the curvature of the lens surfaces).
Fibre Optics
•   Depends upon the total internal reflection of light rays.

•   Light can be trapped by total internal reflection inside a bent glass rod and
    piped along a curved path as in the diagram below. a single, very thin
    glass fiber behaves in the same way.

•   They are small and so, once light is introduced into the fiber with an angle
    within the confines of the numerical aperture of the fiber, it will continue
    to reflect almost losslessly off the walls of the fiber and thus can travel
    long distances in the fiber.

•   If a bundle of parallel fibers is used to construct an optical transmission
    line, images can be transferred from one point to another.
Fibre Optic Imaging


•   Principle : light striking at one end will be transmitted to the other end of
    the fibre.

•   If the arrangement of fibres in the bundle is kept constant then the
    transmitted light forms a mosaic image of the light which struck the end of
    the bundle.
Wave motion
 and sound
Wave motion
•   For example, wave is created at a lake or pond due to disturbance, such as
    a rock thrown into the water.

•   The water wave has a crest and a trough and travels from one location to
    another.

•   One crest is often followed by a second crest which is often followed by a
    third crest, and so on.

•   waves may be circular waves which originate from the point where the
    disturbances occur; such circular waves travel across the surface of the
    water in all directions.
•   Another example, if a slinky is stretched out from end to end, a wave can
    be introduced into the slinky by either vibrating the first coil up and down
    vertically or back and forth horizontally.

•   As the wave moves along the slinky, each individual coil is seen to move
    out of place and then return to its original position.

•   The wave does not stop when it reaches the end of the slinky; rather it
    seems to bounce off the end and head back from where it started.
Categories of Waves
• Waves come in many shapes and forms.
• Some share basic characteristic properties and behaviours, some waves
   can be distinguished from others based on some very observable (and
   some non-observable) characteristics.
• It is common to categorise waves based on these distinguishing
   characteristics.
                                                                  Transverse
                                                                     Wave

                                Direction of movement            Longitudinal
                                                                    wave


                                                                Surface Wave
   To categorize wave

                                                        Electromagnetic Waves
                                 Ability to be
                                 transmitted
                               through vacuum            Mechanical
                                                          Waves
Direction Of Movement
Transverse wave
•   Wave moves in a direction perpendicular to the direction which the wave
    moves.




•   If pulse is applied to the left end by vibrating it up and down, the energy
    will be transported from left to right and particle will be displaced
    upwards and downwards.
Longitudinal Wave


•   Wave in which particles of the medium move in a direction parallel to the
    direction which the wave moves.




•   If force is applied to the left end by vibrating it left and right, the energy
    will be transported from left to right and particle will be displaced
    rightwards and leftwards.
Ability to transmit through vacuum

Electromagnetic Wave
• wave which is capable of transmitting its energy through a vacuum.
• Electromagnetic waves are produced by the vibration of electrons within
    atoms on the Sun's surface.
• These waves subsequently travel through the vacuum of outer space,
    subsequently reaching Earth.
• Eg ; Light Wave.

Mechanical Wave
• Wave which is not capable of transmitting its energy through a vacuum.
• Require a medium in order to transport their energy from one location to
  another.
• Eg ; Sound Wave.
Anatomy of Waves




•     dashed line - equilibrium or rest position of the string.

    (if there were no disturbance moving through it )

•     Points A and F - crests of this wave (point on the medium which exhibits
      the maximum amount of positive or upwards displacement from the rest
      position)

•     Points D and I - troughs of this wave (point on the medium which exhibits
      the maximum amount of negative or downwards displacement from the
      rest position )
•   Amplitude of a wave - maximum amount of displacement of a particle on
    the medium from its rest position. ( from rest to crest )



•   Wavelength ;

          a. Simply the length of one complete wave cycle.

          b. Wave has a repeating pattern. And the length of one such
          repetition (known as a wave cycle) is the wavelength.

          c. Can be measured as the distance from crest to crest or from
trough to trough. ( B – G, E - J, D – I )
Longitudinal wave


•   is a wave in which the particles of the medium are displaced in a direction
    parallel to the direction of energy transport.

•   Wavelength - determined by measuring the distance between any two
    corresponding points on adjacent waves. ( measure distance from a
    compression to the next compression or from a rarefaction to the next
    rarefaction ; A – C , B – D )
Frequency and Period of a Wave

•   Frequency ;
          a. refers to how often the particles of the medium vibrate when a
wave passes through the medium.
          b. number of complete vibration cycles of a medium per a given
amount of time and it as the units of cycles per second      or Hertz (Hz)
where 1 Hz is equivalent to 1 cycle/second.
          c. . A detector could be used to detect the frequency of these
          pressure oscillations over a given period of time.
          d. unit : Hertz, Hz ( cycle / sec )
• Period ;
          a. the time which it takes to do something.
          b. the time for a particle on a medium to make one complete
          vibration cycle.
          c. When an event occurs repeatedly, then we say that the event is
periodic.
          d. measured in units of time such as seconds, hours, days or
          years.
Interference Phenomena

Wave interference
• phenomenon which occurs when two waves meet while travelling along
  the same medium.




•   Causes the medium to take on a shape which results from the net effect of
    the two individual waves upon the particles of the medium.
•   Eg ; if 2 crests of wave having amplitude of +1 move into each other, the
    resulting sine crest +2 is created at the moment when the 2 waves
    overlapped.
•   Sometimes called Constructive Interference.
Constructive Interference


•   Occurs at any location along the medium where the two interfering waves
    have a displacement in the same direction.

•   If both waves have an upward displacement; consequently, the medium
    has an upward displacement which is greater than the displacement of the
    two interfering pulses.
Destructive Interference

•   type of interference which occurs at any location along the medium where
    the two interfering waves have a displacement in the opposite direction.




•   If a sine crest with an amplitude of +1 unit meets a sine trough with an
    amplitude of -1 unit, destructive interference occurs.
•   The two pulses cancel each other for the duration of the overlap.
•    Once the two pulses pass through each other, there is still a crest and a
    trough heading in the same direction which they were heading before
    interference.
Principle of Superposition
“When two waves interfere, the resulting displacement of the medium at any
location is the algebraic sum of the displacements of the individual waves at that
same location.”
•   To determine the shape of the resultant wave caused by the interference of
    two separate waves.
•   Standing Wave pattern :
               An interference phenomena.
               When the vibration frequency of the source causes
                  reflected waves from one end of the medium to interfere
                  with incident waves from the source in such a manner
                  that specific points along the medium appear to be
                  standing still.
               Only created within the medium at specific frequencies of
                  vibration; these frequencies are known as harmonic
                  frequencies, or merely harmonics.
               From the presence of two waves (sometimes more) of the
                  same frequency with different directions of travel within
•   Anti-nodes - point A on the medium moves from a positive to a negative
    displacement over time.

•   Nodes - point B on the medium is a point which never moves.
Standing Wave
•   stationary wave - is a wave that remains in a constant position.
•   often applied to a resonant mode of an extended vibrating object.
•   created by constructive interference of two waves which travel in opposite
    directions in the medium, but the visual effect is that of an entire system
    moving in simple harmonic motion.
•   modes of vibration associated with resonance in extended objects like
    strings and air columns have characteristic patterns called standing waves.
•   arise from the combination of reflection and interference such that the
    reflected waves interfere constructively with the incident waves.
•   An important part of the condition for this constructive interference for
    stretched strings is the fact that the waves change phase upon reflection
    from a fixed end.
Sound
• Sound wave - pressure disturbance which travels through a medium by
   means of particle interaction.
• As one particle becomes disturbed, it exerts a force on the next adjacent
   particle, thus disturbing that particle from rest and transporting the
   energy through the medium.
• speed of a sound wave refers to how fast the disturbance is passed from
   particle to particle.
• frequency refers to the number of vibrations which an individual particle
   makes per unit of time.
• speed refers to the distance which the disturbance travels per unit of time.
Speed of Sound
•   Is determined to be 331 ½ m / s at 00C – 1087 ft /s , 741 mph or 644 kts.
•   liquids are better transmitters of sound.
•   Eg. sound waves travel approx. 4 times faster in water than in air and
    speed of sound in solids is even greater, sound travels through steel is 15
    times faster than it travels in air.
          speed ( sound wave ) = frequency x wavelength
•   Alteration in wavelength effects the frequency, but not the wave speed.
•   Doubling of wavelength results in halving the frequency, but wave speed
    doe not change.
•   The speed of sound wave depends on the properties of the medium
    through which it moves.
•   Primarily affected by temperature, the lower the temperature, the lower
    the speed of sound.

                   speed of sound = √ ( γ R T )

          where    γ = ratio of specific heats of the gas

                    R = gas constant

                    T = gas temperature ( in Kelvin )

•   It determines the nature and formation of shock waves.

          Mach No = True Airspeed of aircraft

                              Speed Of Sound
Intensity
•   amount of energy which is transported past a given area of the medium per unit of
    time.

•   Often referred to as ‘loudness’ , the energy of the wave.

•   The greater the amplitude of vibrations of the particles of the medium, the greater the
    rate at which energy is transported through it, and the more intense that the sound
    wave is.

•   Intensity is the energy/time/area; and since the energy/time ratio is equivalent to the
    quantity power, intensity is simply the power/area.

            Intensity = Energy           or Intensity = Power

                        Time x Area                       Area

•   Eg ; if amplitude of sound wave is doubled, intensity will increase fourfold.

•   Unit : Watts / Meter2 . But scale to measure intensity; Desibel (dB)
Pitch
• Best described as position on musical scale.
•   The ears of humans (and other animals) are sensitive detectors capable of
    detecting the fluctuations in air pressure which impinge upon the
    eardrum.

•   The human ear is capable of detecting sound waves with a wide range of
    frequencies, ranging between approximately 20 Hz to 20 000 Hz.

•   The sensations of these frequencies are commonly referred to as the
    pitch.

•   A high pitch sound corresponds to a high frequency and a low pitch sound
    corresponds to a low frequency.
Doppler Effect




•   effect produced by a moving source of waves in which there is an
    apparent upward shift in frequency for the observer and the source are
    approaching and an apparent downward shift in frequency when the
    observer and the source is receding.
•   Occur with all types of waves - most notably water waves, sound waves,
    and light waves.
•   Doppler Effect observed because the distance between the source of sound and the
    observer is changing.




•   If the source and the observer are approaching, then the distance is decreasing and if
    the source and the observer are receding, then the distance is increasing.
•   If the source is moving towards the observer, the observer perceives sound waves
    reaching him or her at a more frequent rate (high pitch); and if the source is moving
    away from the observer, the observer perceives sound waves reaching him or her at
    a less frequent rate (low pitch).

Weitere ähnliche Inhalte

Was ist angesagt?

EASA Part-66 Module08 mcq's
EASA Part-66 Module08 mcq'sEASA Part-66 Module08 mcq's
EASA Part-66 Module08 mcq'sArmghan Saeed
 
UNIT - III NORMAL & OBLIQUE SHOCKS
UNIT - III NORMAL & OBLIQUE SHOCKSUNIT - III NORMAL & OBLIQUE SHOCKS
UNIT - III NORMAL & OBLIQUE SHOCKSsureshkcet
 
EASA PART-66 MODULE 5.3 : DATA CONVERSION
EASA PART-66 MODULE 5.3 : DATA CONVERSIONEASA PART-66 MODULE 5.3 : DATA CONVERSION
EASA PART-66 MODULE 5.3 : DATA CONVERSIONsoulstalker
 
Aircraft landing gear system
Aircraft landing gear systemAircraft landing gear system
Aircraft landing gear systemKrishikesh Singh
 
EASA Part-66 Module04 mcq's
EASA Part-66 Module04 mcq'sEASA Part-66 Module04 mcq's
EASA Part-66 Module04 mcq'sArmghan Saeed
 
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMS
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMSEASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMS
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMSsoulstalker
 
Aircraft materials and hardware
Aircraft materials and hardwareAircraft materials and hardware
Aircraft materials and hardwareShan-go Gratien
 
Aerodynamic theories
Aerodynamic theoriesAerodynamic theories
Aerodynamic theoriessadir44503
 
EASA Part-66 Module02 mcq's
EASA Part-66 Module02 mcq'sEASA Part-66 Module02 mcq's
EASA Part-66 Module02 mcq'sArmghan Saeed
 
Airframe Maintenance and Repair
Airframe Maintenance and RepairAirframe Maintenance and Repair
Airframe Maintenance and RepairDeepanBooramurthy
 
EASA Part-66 Module07 mcq's
EASA Part-66 Module07 mcq'sEASA Part-66 Module07 mcq's
EASA Part-66 Module07 mcq'sArmghan Saeed
 
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...Age of Aerospace
 
EASA Part 66 Module 15.2 : Engine Performance
EASA Part 66 Module 15.2 : Engine PerformanceEASA Part 66 Module 15.2 : Engine Performance
EASA Part 66 Module 15.2 : Engine Performancesoulstalker
 
CFD analysis of aerofoil
CFD analysis of aerofoilCFD analysis of aerofoil
CFD analysis of aerofoilNeel Thakkar
 
EASA PART-66 MODULE 5.4 : DATA BUSES
EASA PART-66 MODULE 5.4 : DATA BUSESEASA PART-66 MODULE 5.4 : DATA BUSES
EASA PART-66 MODULE 5.4 : DATA BUSESsoulstalker
 

Was ist angesagt? (20)

EASA Part-66 Module08 mcq's
EASA Part-66 Module08 mcq'sEASA Part-66 Module08 mcq's
EASA Part-66 Module08 mcq's
 
UNIT - III NORMAL & OBLIQUE SHOCKS
UNIT - III NORMAL & OBLIQUE SHOCKSUNIT - III NORMAL & OBLIQUE SHOCKS
UNIT - III NORMAL & OBLIQUE SHOCKS
 
EASA PART-66 MODULE 5.3 : DATA CONVERSION
EASA PART-66 MODULE 5.3 : DATA CONVERSIONEASA PART-66 MODULE 5.3 : DATA CONVERSION
EASA PART-66 MODULE 5.3 : DATA CONVERSION
 
Aircraft landing gear system
Aircraft landing gear systemAircraft landing gear system
Aircraft landing gear system
 
Aircraft Wing
Aircraft Wing Aircraft Wing
Aircraft Wing
 
EASA Part-66 Module04 mcq's
EASA Part-66 Module04 mcq'sEASA Part-66 Module04 mcq's
EASA Part-66 Module04 mcq's
 
Aerodynamics slide
Aerodynamics slideAerodynamics slide
Aerodynamics slide
 
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMS
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMSEASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMS
EASA PART-66 MODULE 5.15 : TYPICAL AIRCRAFT INSTRUMENT SYSTEMS
 
Types of drag
Types of dragTypes of drag
Types of drag
 
Aircraft materials and hardware
Aircraft materials and hardwareAircraft materials and hardware
Aircraft materials and hardware
 
Aerodynamic theories
Aerodynamic theoriesAerodynamic theories
Aerodynamic theories
 
EASA Part-66 Module02 mcq's
EASA Part-66 Module02 mcq'sEASA Part-66 Module02 mcq's
EASA Part-66 Module02 mcq's
 
Airframe Maintenance and Repair
Airframe Maintenance and RepairAirframe Maintenance and Repair
Airframe Maintenance and Repair
 
Aircraft wing
Aircraft wingAircraft wing
Aircraft wing
 
EASA Part-66 Module07 mcq's
EASA Part-66 Module07 mcq'sEASA Part-66 Module07 mcq's
EASA Part-66 Module07 mcq's
 
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...
Atmosphere: Properties and Standard Atmosphere | Flight Mechanics | GATE Aero...
 
EASA Part 66 Module 15.2 : Engine Performance
EASA Part 66 Module 15.2 : Engine PerformanceEASA Part 66 Module 15.2 : Engine Performance
EASA Part 66 Module 15.2 : Engine Performance
 
CFD analysis of aerofoil
CFD analysis of aerofoilCFD analysis of aerofoil
CFD analysis of aerofoil
 
EASA PART-66 MODULE 5.4 : DATA BUSES
EASA PART-66 MODULE 5.4 : DATA BUSESEASA PART-66 MODULE 5.4 : DATA BUSES
EASA PART-66 MODULE 5.4 : DATA BUSES
 
Hydraulic system of landing gear in Aircraft
Hydraulic system of landing gear in Aircraft Hydraulic system of landing gear in Aircraft
Hydraulic system of landing gear in Aircraft
 

Andere mochten auch

EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICSEASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICSsoulstalker
 
Ch19 Electric Potential Energy and Electric Potential
Ch19 Electric Potential Energy and Electric PotentialCh19 Electric Potential Energy and Electric Potential
Ch19 Electric Potential Energy and Electric PotentialScott Thomas
 
Work and electric potential lecture # physics 2
Work and electric potential lecture # physics 2Work and electric potential lecture # physics 2
Work and electric potential lecture # physics 2Denmar Marasigan
 
9.3 - Electric Potential
9.3 - Electric Potential9.3 - Electric Potential
9.3 - Electric Potentialsimonandisa
 
General Physics (2) lect 1
General Physics (2) lect 1General Physics (2) lect 1
General Physics (2) lect 1Dr. Abeer Kamal
 
AP Phnysics - Chapter 19 Powerpoint
AP Phnysics - Chapter 19 PowerpointAP Phnysics - Chapter 19 Powerpoint
AP Phnysics - Chapter 19 PowerpointMrreynon
 
Physics - Chapter 2 - One Dimensional Motion
Physics - Chapter 2 - One Dimensional MotionPhysics - Chapter 2 - One Dimensional Motion
Physics - Chapter 2 - One Dimensional MotionJPoilek
 
Ch10 - potential difference and electric potential energy
Ch10  - potential difference and electric potential energyCh10  - potential difference and electric potential energy
Ch10 - potential difference and electric potential energycpphysics
 
EASA PART 66 Module 15.10 : Lubrication Systems
EASA PART 66 Module 15.10 : Lubrication SystemsEASA PART 66 Module 15.10 : Lubrication Systems
EASA PART 66 Module 15.10 : Lubrication Systemssoulstalker
 
Physics Unit P2
Physics Unit P2Physics Unit P2
Physics Unit P2Louisatom
 
Electric potential difference (voltage)
Electric potential difference (voltage)Electric potential difference (voltage)
Electric potential difference (voltage)Jean Tralala
 
Test Automation - Principles and Practices
Test Automation - Principles and PracticesTest Automation - Principles and Practices
Test Automation - Principles and PracticesAnand Bagmar
 
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMS
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMSEASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMS
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMSsoulstalker
 

Andere mochten auch (17)

Atpl book-2-airframes-and-systems
Atpl book-2-airframes-and-systemsAtpl book-2-airframes-and-systems
Atpl book-2-airframes-and-systems
 
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICSEASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
EASA PART-66 MODULE 8.4 : FLIGHT STABILITY AND DYNAMICS
 
Ch19 Electric Potential Energy and Electric Potential
Ch19 Electric Potential Energy and Electric PotentialCh19 Electric Potential Energy and Electric Potential
Ch19 Electric Potential Energy and Electric Potential
 
Work and electric potential lecture # physics 2
Work and electric potential lecture # physics 2Work and electric potential lecture # physics 2
Work and electric potential lecture # physics 2
 
General physics-i 18
General physics-i 18General physics-i 18
General physics-i 18
 
9.3 - Electric Potential
9.3 - Electric Potential9.3 - Electric Potential
9.3 - Electric Potential
 
General Physics (2) lect 1
General Physics (2) lect 1General Physics (2) lect 1
General Physics (2) lect 1
 
AP Phnysics - Chapter 19 Powerpoint
AP Phnysics - Chapter 19 PowerpointAP Phnysics - Chapter 19 Powerpoint
AP Phnysics - Chapter 19 Powerpoint
 
Electric potential
Electric potentialElectric potential
Electric potential
 
Physics - Chapter 2 - One Dimensional Motion
Physics - Chapter 2 - One Dimensional MotionPhysics - Chapter 2 - One Dimensional Motion
Physics - Chapter 2 - One Dimensional Motion
 
Ch10 - potential difference and electric potential energy
Ch10  - potential difference and electric potential energyCh10  - potential difference and electric potential energy
Ch10 - potential difference and electric potential energy
 
EASA PART 66 Module 15.10 : Lubrication Systems
EASA PART 66 Module 15.10 : Lubrication SystemsEASA PART 66 Module 15.10 : Lubrication Systems
EASA PART 66 Module 15.10 : Lubrication Systems
 
Physics Unit P2
Physics Unit P2Physics Unit P2
Physics Unit P2
 
Electric potential difference (voltage)
Electric potential difference (voltage)Electric potential difference (voltage)
Electric potential difference (voltage)
 
General physics
General physicsGeneral physics
General physics
 
Test Automation - Principles and Practices
Test Automation - Principles and PracticesTest Automation - Principles and Practices
Test Automation - Principles and Practices
 
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMS
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMSEASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMS
EASA PART 66 MODULE 5.1 : ELECTRONIC INSTRUMENT SYSTEMS
 

Ähnlich wie PHYSICS MODULE 2: BASIC CONCEPTS

Physicclass easa part 66
Physicclass easa part 66Physicclass easa part 66
Physicclass easa part 66S Qasim Naqvi
 
Physic Module PPT
Physic Module PPTPhysic Module PPT
Physic Module PPTboysarena
 
Periodic Trends Complete.ppt
Periodic Trends Complete.pptPeriodic Trends Complete.ppt
Periodic Trends Complete.pptthemmendoza
 
Chapter 9 atoms and the periodic table
Chapter 9 atoms and the periodic tableChapter 9 atoms and the periodic table
Chapter 9 atoms and the periodic tablecoolscienceguy
 
1. introduction and basic definitions.pf
1. introduction and basic definitions.pf1. introduction and basic definitions.pf
1. introduction and basic definitions.pf9cp7wp28kx
 
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptx
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptxchap 1 Chapter 1 chapter1 chapter1 chapter 1.pptx
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptxTaroTari
 
Resume physic success sat
Resume physic success satResume physic success sat
Resume physic success satAri Almeida
 
Kmt, intermolecular forces, intro energy
Kmt, intermolecular forces, intro energyKmt, intermolecular forces, intro energy
Kmt, intermolecular forces, intro energyFelipe De la Garza
 
A++ mission 6 notes part i 2012
A++ mission 6 notes part i 2012A++ mission 6 notes part i 2012
A++ mission 6 notes part i 2012Don Wade
 
Basic Atomic structure
Basic Atomic structureBasic Atomic structure
Basic Atomic structureVinay Desai
 
atomicstructurevinay-161206190926.pdf
atomicstructurevinay-161206190926.pdfatomicstructurevinay-161206190926.pdf
atomicstructurevinay-161206190926.pdfUmerImran14
 
atomicstructurevinay-161206190926 (1).pptx
atomicstructurevinay-161206190926 (1).pptxatomicstructurevinay-161206190926 (1).pptx
atomicstructurevinay-161206190926 (1).pptxnorthernsamarjbbinam
 

Ähnlich wie PHYSICS MODULE 2: BASIC CONCEPTS (20)

Physicclass easa part 66
Physicclass easa part 66Physicclass easa part 66
Physicclass easa part 66
 
Physic Module PPT
Physic Module PPTPhysic Module PPT
Physic Module PPT
 
structure of atom
structure of atomstructure of atom
structure of atom
 
structure of atom
structure of atomstructure of atom
structure of atom
 
Review
ReviewReview
Review
 
Periodic Trends Complete.ppt
Periodic Trends Complete.pptPeriodic Trends Complete.ppt
Periodic Trends Complete.ppt
 
Chapter 9 atoms and the periodic table
Chapter 9 atoms and the periodic tableChapter 9 atoms and the periodic table
Chapter 9 atoms and the periodic table
 
1. introduction and basic definitions.pf
1. introduction and basic definitions.pf1. introduction and basic definitions.pf
1. introduction and basic definitions.pf
 
Human Physiology Chemistry
Human Physiology ChemistryHuman Physiology Chemistry
Human Physiology Chemistry
 
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptx
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptxchap 1 Chapter 1 chapter1 chapter1 chapter 1.pptx
chap 1 Chapter 1 chapter1 chapter1 chapter 1.pptx
 
Resume physic success sat
Resume physic success satResume physic success sat
Resume physic success sat
 
Nuclear chemistry
Nuclear chemistryNuclear chemistry
Nuclear chemistry
 
Kmt, intermolecular forces, intro energy
Kmt, intermolecular forces, intro energyKmt, intermolecular forces, intro energy
Kmt, intermolecular forces, intro energy
 
Mass spectrometry
Mass spectrometryMass spectrometry
Mass spectrometry
 
A++ mission 6 notes part i 2012
A++ mission 6 notes part i 2012A++ mission 6 notes part i 2012
A++ mission 6 notes part i 2012
 
Lecture 4 (1)
Lecture 4 (1)Lecture 4 (1)
Lecture 4 (1)
 
Chemistry Basics
Chemistry BasicsChemistry Basics
Chemistry Basics
 
Basic Atomic structure
Basic Atomic structureBasic Atomic structure
Basic Atomic structure
 
atomicstructurevinay-161206190926.pdf
atomicstructurevinay-161206190926.pdfatomicstructurevinay-161206190926.pdf
atomicstructurevinay-161206190926.pdf
 
atomicstructurevinay-161206190926 (1).pptx
atomicstructurevinay-161206190926 (1).pptxatomicstructurevinay-161206190926 (1).pptx
atomicstructurevinay-161206190926 (1).pptx
 

Mehr von soulstalker

EASA Part 66 Module 15.8 : Bearings and Seals
EASA Part 66 Module 15.8 : Bearings and Seals EASA Part 66 Module 15.8 : Bearings and Seals
EASA Part 66 Module 15.8 : Bearings and Seals soulstalker
 
EASA Part 66 Module 15.7 : Exhausts
EASA Part 66 Module 15.7 : ExhaustsEASA Part 66 Module 15.7 : Exhausts
EASA Part 66 Module 15.7 : Exhaustssoulstalker
 
EASA Part 66 Module 15.6 : Turbine
EASA Part 66 Module 15.6 : TurbineEASA Part 66 Module 15.6 : Turbine
EASA Part 66 Module 15.6 : Turbinesoulstalker
 
EASA Part 66 Module 15.5 : Combustion Chamber
EASA Part 66 Module 15.5 : Combustion ChamberEASA Part 66 Module 15.5 : Combustion Chamber
EASA Part 66 Module 15.5 : Combustion Chambersoulstalker
 
EASA Part 66 Module 15.4 : Compressors
EASA Part 66 Module 15.4 : CompressorsEASA Part 66 Module 15.4 : Compressors
EASA Part 66 Module 15.4 : Compressorssoulstalker
 
EASA Part 66 Module 15.3 : Inlet
EASA Part 66 Module 15.3 : InletEASA Part 66 Module 15.3 : Inlet
EASA Part 66 Module 15.3 : Inletsoulstalker
 
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENTEASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENTsoulstalker
 
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICES
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICESEASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICES
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICESsoulstalker
 
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYS
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYSEASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYS
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYSsoulstalker
 
EASA Part-66 Module 5.6 : Basic Computer Structure
EASA Part-66 Module  5.6 : Basic Computer StructureEASA Part-66 Module  5.6 : Basic Computer Structure
EASA Part-66 Module 5.6 : Basic Computer Structuresoulstalker
 
EASA Part 66 Module 5.13 : Software Management Control
EASA Part 66 Module 5.13 : Software Management ControlEASA Part 66 Module 5.13 : Software Management Control
EASA Part 66 Module 5.13 : Software Management Controlsoulstalker
 
EASA Part 66 Module 5.10 : Fibre Optic
EASA Part 66 Module 5.10 : Fibre OpticEASA Part 66 Module 5.10 : Fibre Optic
EASA Part 66 Module 5.10 : Fibre Opticsoulstalker
 
EASA Part 66 Module 5.5 : Logic Circuit
EASA Part 66 Module 5.5 : Logic CircuitEASA Part 66 Module 5.5 : Logic Circuit
EASA Part 66 Module 5.5 : Logic Circuitsoulstalker
 
EASA Part 66 Module 5.2 : Numbering System
EASA Part 66 Module 5.2 : Numbering SystemEASA Part 66 Module 5.2 : Numbering System
EASA Part 66 Module 5.2 : Numbering Systemsoulstalker
 

Mehr von soulstalker (14)

EASA Part 66 Module 15.8 : Bearings and Seals
EASA Part 66 Module 15.8 : Bearings and Seals EASA Part 66 Module 15.8 : Bearings and Seals
EASA Part 66 Module 15.8 : Bearings and Seals
 
EASA Part 66 Module 15.7 : Exhausts
EASA Part 66 Module 15.7 : ExhaustsEASA Part 66 Module 15.7 : Exhausts
EASA Part 66 Module 15.7 : Exhausts
 
EASA Part 66 Module 15.6 : Turbine
EASA Part 66 Module 15.6 : TurbineEASA Part 66 Module 15.6 : Turbine
EASA Part 66 Module 15.6 : Turbine
 
EASA Part 66 Module 15.5 : Combustion Chamber
EASA Part 66 Module 15.5 : Combustion ChamberEASA Part 66 Module 15.5 : Combustion Chamber
EASA Part 66 Module 15.5 : Combustion Chamber
 
EASA Part 66 Module 15.4 : Compressors
EASA Part 66 Module 15.4 : CompressorsEASA Part 66 Module 15.4 : Compressors
EASA Part 66 Module 15.4 : Compressors
 
EASA Part 66 Module 15.3 : Inlet
EASA Part 66 Module 15.3 : InletEASA Part 66 Module 15.3 : Inlet
EASA Part 66 Module 15.3 : Inlet
 
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENTEASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT
EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT
 
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICES
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICESEASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICES
EASA PART-66 MODULE 5.12 : ELECTRONICS SENSITIVE DEVICES
 
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYS
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYSEASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYS
EASA PART-66 MODULE 5.11 : ELECTRONIC DISPLAYS
 
EASA Part-66 Module 5.6 : Basic Computer Structure
EASA Part-66 Module  5.6 : Basic Computer StructureEASA Part-66 Module  5.6 : Basic Computer Structure
EASA Part-66 Module 5.6 : Basic Computer Structure
 
EASA Part 66 Module 5.13 : Software Management Control
EASA Part 66 Module 5.13 : Software Management ControlEASA Part 66 Module 5.13 : Software Management Control
EASA Part 66 Module 5.13 : Software Management Control
 
EASA Part 66 Module 5.10 : Fibre Optic
EASA Part 66 Module 5.10 : Fibre OpticEASA Part 66 Module 5.10 : Fibre Optic
EASA Part 66 Module 5.10 : Fibre Optic
 
EASA Part 66 Module 5.5 : Logic Circuit
EASA Part 66 Module 5.5 : Logic CircuitEASA Part 66 Module 5.5 : Logic Circuit
EASA Part 66 Module 5.5 : Logic Circuit
 
EASA Part 66 Module 5.2 : Numbering System
EASA Part 66 Module 5.2 : Numbering SystemEASA Part 66 Module 5.2 : Numbering System
EASA Part 66 Module 5.2 : Numbering System
 

Kürzlich hochgeladen

Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptx
Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptxQ4-PPT-Music9_Lesson-1-Romantic-Opera.pptx
Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptxlancelewisportillo
 
4.18.24 Movement Legacies, Reflection, and Review.pptx
4.18.24 Movement Legacies, Reflection, and Review.pptx4.18.24 Movement Legacies, Reflection, and Review.pptx
4.18.24 Movement Legacies, Reflection, and Review.pptxmary850239
 
Influencing policy (training slides from Fast Track Impact)
Influencing policy (training slides from Fast Track Impact)Influencing policy (training slides from Fast Track Impact)
Influencing policy (training slides from Fast Track Impact)Mark Reed
 
Choosing the Right CBSE School A Comprehensive Guide for Parents
Choosing the Right CBSE School A Comprehensive Guide for ParentsChoosing the Right CBSE School A Comprehensive Guide for Parents
Choosing the Right CBSE School A Comprehensive Guide for Parentsnavabharathschool99
 
ROLES IN A STAGE PRODUCTION in arts.pptx
ROLES IN A STAGE PRODUCTION in arts.pptxROLES IN A STAGE PRODUCTION in arts.pptx
ROLES IN A STAGE PRODUCTION in arts.pptxVanesaIglesias10
 
Daily Lesson Plan in Mathematics Quarter 4
Daily Lesson Plan in Mathematics Quarter 4Daily Lesson Plan in Mathematics Quarter 4
Daily Lesson Plan in Mathematics Quarter 4JOYLYNSAMANIEGO
 
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...Postal Advocate Inc.
 
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)lakshayb543
 
Activity 2-unit 2-update 2024. English translation
Activity 2-unit 2-update 2024. English translationActivity 2-unit 2-update 2024. English translation
Activity 2-unit 2-update 2024. English translationRosabel UA
 
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptx
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptxMULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptx
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptxAnupkumar Sharma
 
Earth Day Presentation wow hello nice great
Earth Day Presentation wow hello nice greatEarth Day Presentation wow hello nice great
Earth Day Presentation wow hello nice greatYousafMalik24
 
Student Profile Sample - We help schools to connect the data they have, with ...
Student Profile Sample - We help schools to connect the data they have, with ...Student Profile Sample - We help schools to connect the data they have, with ...
Student Profile Sample - We help schools to connect the data they have, with ...Seán Kennedy
 
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITY
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITYISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITY
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITYKayeClaireEstoconing
 
Barangay Council for the Protection of Children (BCPC) Orientation.pptx
Barangay Council for the Protection of Children (BCPC) Orientation.pptxBarangay Council for the Protection of Children (BCPC) Orientation.pptx
Barangay Council for the Protection of Children (BCPC) Orientation.pptxCarlos105
 
How to do quick user assign in kanban in Odoo 17 ERP
How to do quick user assign in kanban in Odoo 17 ERPHow to do quick user assign in kanban in Odoo 17 ERP
How to do quick user assign in kanban in Odoo 17 ERPCeline George
 
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...JhezDiaz1
 
Keynote by Prof. Wurzer at Nordex about IP-design
Keynote by Prof. Wurzer at Nordex about IP-designKeynote by Prof. Wurzer at Nordex about IP-design
Keynote by Prof. Wurzer at Nordex about IP-designMIPLM
 

Kürzlich hochgeladen (20)

FINALS_OF_LEFT_ON_C'N_EL_DORADO_2024.pptx
FINALS_OF_LEFT_ON_C'N_EL_DORADO_2024.pptxFINALS_OF_LEFT_ON_C'N_EL_DORADO_2024.pptx
FINALS_OF_LEFT_ON_C'N_EL_DORADO_2024.pptx
 
Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptx
Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptxQ4-PPT-Music9_Lesson-1-Romantic-Opera.pptx
Q4-PPT-Music9_Lesson-1-Romantic-Opera.pptx
 
4.18.24 Movement Legacies, Reflection, and Review.pptx
4.18.24 Movement Legacies, Reflection, and Review.pptx4.18.24 Movement Legacies, Reflection, and Review.pptx
4.18.24 Movement Legacies, Reflection, and Review.pptx
 
Influencing policy (training slides from Fast Track Impact)
Influencing policy (training slides from Fast Track Impact)Influencing policy (training slides from Fast Track Impact)
Influencing policy (training slides from Fast Track Impact)
 
LEFT_ON_C'N_ PRELIMS_EL_DORADO_2024.pptx
LEFT_ON_C'N_ PRELIMS_EL_DORADO_2024.pptxLEFT_ON_C'N_ PRELIMS_EL_DORADO_2024.pptx
LEFT_ON_C'N_ PRELIMS_EL_DORADO_2024.pptx
 
Choosing the Right CBSE School A Comprehensive Guide for Parents
Choosing the Right CBSE School A Comprehensive Guide for ParentsChoosing the Right CBSE School A Comprehensive Guide for Parents
Choosing the Right CBSE School A Comprehensive Guide for Parents
 
ROLES IN A STAGE PRODUCTION in arts.pptx
ROLES IN A STAGE PRODUCTION in arts.pptxROLES IN A STAGE PRODUCTION in arts.pptx
ROLES IN A STAGE PRODUCTION in arts.pptx
 
Daily Lesson Plan in Mathematics Quarter 4
Daily Lesson Plan in Mathematics Quarter 4Daily Lesson Plan in Mathematics Quarter 4
Daily Lesson Plan in Mathematics Quarter 4
 
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...
USPS® Forced Meter Migration - How to Know if Your Postage Meter Will Soon be...
 
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)
Visit to a blind student's school🧑‍🦯🧑‍🦯(community medicine)
 
Activity 2-unit 2-update 2024. English translation
Activity 2-unit 2-update 2024. English translationActivity 2-unit 2-update 2024. English translation
Activity 2-unit 2-update 2024. English translation
 
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptx
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptxMULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptx
MULTIDISCIPLINRY NATURE OF THE ENVIRONMENTAL STUDIES.pptx
 
YOUVE GOT EMAIL_FINALS_EL_DORADO_2024.pptx
YOUVE GOT EMAIL_FINALS_EL_DORADO_2024.pptxYOUVE GOT EMAIL_FINALS_EL_DORADO_2024.pptx
YOUVE GOT EMAIL_FINALS_EL_DORADO_2024.pptx
 
Earth Day Presentation wow hello nice great
Earth Day Presentation wow hello nice greatEarth Day Presentation wow hello nice great
Earth Day Presentation wow hello nice great
 
Student Profile Sample - We help schools to connect the data they have, with ...
Student Profile Sample - We help schools to connect the data they have, with ...Student Profile Sample - We help schools to connect the data they have, with ...
Student Profile Sample - We help schools to connect the data they have, with ...
 
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITY
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITYISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITY
ISYU TUNGKOL SA SEKSWLADIDA (ISSUE ABOUT SEXUALITY
 
Barangay Council for the Protection of Children (BCPC) Orientation.pptx
Barangay Council for the Protection of Children (BCPC) Orientation.pptxBarangay Council for the Protection of Children (BCPC) Orientation.pptx
Barangay Council for the Protection of Children (BCPC) Orientation.pptx
 
How to do quick user assign in kanban in Odoo 17 ERP
How to do quick user assign in kanban in Odoo 17 ERPHow to do quick user assign in kanban in Odoo 17 ERP
How to do quick user assign in kanban in Odoo 17 ERP
 
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...
ENGLISH 7_Q4_LESSON 2_ Employing a Variety of Strategies for Effective Interp...
 
Keynote by Prof. Wurzer at Nordex about IP-design
Keynote by Prof. Wurzer at Nordex about IP-designKeynote by Prof. Wurzer at Nordex about IP-design
Keynote by Prof. Wurzer at Nordex about IP-design
 

PHYSICS MODULE 2: BASIC CONCEPTS

  • 1. PHYSICS MODULE 2 www.part66.blogspot.com
  • 2. Basic SI Units Length (L) Metre (m) Mass (m) Kilogram(kg) Time (t) Second (s) Derived SI Units Area (A) Square Metre (m2) Volume (V) Cubic Metre (m3) Density (ρ) Kg / Cubic Metre (kg/m3) Velocity (V) Metre per second (m/s) Force (F) Newton (N) Pressure(p) Pascal (Pa) Energy (E) Joule (J) Work (W) Joule (J) Power (P) Watt (w) Frequency(f) Hertz (Hz)
  • 3. matter • Matter - anything that occupies space. - consists of atoms and molecules. • Atom - smallest particle in an element that has the properties of the element. • Molecules - the combination of two or more atoms.
  • 4. NATURE OF MATTER • Nucleus - each carrying a positive charge are called protons. In addition to the protons the nucleus usually contains electrically neutral particles called neutrons. Neutrons have the same mass as protons whereas electrons are very much smaller. • Neutron - simply adds to the weight of the nucleus. - has no charge. • Proton - positively charged. - has mass same as the neutrons. • Electron - orbits define the size or volume occupied by the atom - negatively charged. - total number of negatively charged electrons matches number of positively charged protons.
  • 5.
  • 6. • The sub-atomic components of atoms. Particles Relative Electrical Comments Mass Charge Neutron 1 0 ( zero ) In the nucleus Proton 1 +1 ( positive ) In the nucleus Electron 1 / 1850 -1 ( negative ) Arranged in energy levels or shells around the nucleus
  • 7. • Atomic Number – no. of protons in the atom’s nucleus. eg. Hydrogen has 1 proton – atomic no. is 1. Carbon has 6 protons – atomic no. is 6. • Mass Number – total no. of protons and neutrons in nucleus. eg. Lithium has 3 protons & 4 neutrons – mass no. 7
  • 8. Relative Atomic Mass The mass of atom in relation to the mass of a reference atom. Element chosen on which to relate mass of all atoms is Carbon. Eg. Carbon (12) - 6 protons + 6 neutrons Hydrogen - 1 proton + 0 neutron = mass no. 1 *so relative atomic mass for Hydrogen is one twelfth of Carbon.
  • 9.
  • 10. Isotopes • are atoms that have same atomic number but different mass numbers. • Atom gains / loses one or more neutrons from nucleus will become ISOTOPES. • Are present in most elements and may also be man made.
  • 11.
  • 12. • From left to right across a period = protons/electrons count increases by one. • Atomic number = increases from left to right. • Group 1. Vertical column 2. Elements have same number of outer shell / valency electrons. Noble gases - group 8. Transition metals - middle of the table. Pure metals - group 1, except Hydrogen.
  • 13. CHEMICAL COMPOUNDS • Atoms bond together to form a molecule. Molecules Monatomic Molecule Chemical Compounds Consists of single type of atom. Made up of two or more atoms.
  • 14. Structure of Atoms • Electrons are arranged in energy levels and shells around the nucleus and with increasing distance from the nucleus . • Valence electrons : - how many electrons an atom has in its outer shell. - determines the chemical behavior. - The more valence electrons, the more want for the atom to get more electrons. • Valency : 1. bonding capacity of an atom; usually equals the number of unpaired electrons in the atoms outermost shell. 2. No. of bonds it can make with a monovalent atom such as Hydrogen. Monovalent Bivalent Trivalent Tetravalent
  • 15. The Molecule • A group of two or more similar or dissimilar atoms bonded together . • Metallic bonds - metal + metal (eg: Alloy) - do not produce molecules - weakest bonds of all • Ionic bonds - metal + non-metal (eg: sodium chloride) • Covalent bonds - non metal + non metal (eg : water) - produce molecules, strongest bond.
  • 16. Chemical compounds • Defined as : ‘ A substance made up of different elements that are chemically bonded and are so united that the whole has properties of its own, which are unlike those of its constituents.’ • All other molecules made up of two or more atoms are known as Chemical compound.
  • 17. States of matter • All matter exists in one of three physical states. • Physical state refers to the condition of a compound and has no affect on a compound's chemical structure. • Solid. A solid has definite mass, volume and shape. • Liquid. A liquid has definite mass and volume but takes the shape of its container. • Gas. A gas has definite mass but takes the volume and shape of its container. • increase in the temperature will increase the energy of its molecules.
  • 18.
  • 19. Changes between states • Solid to Liquid – Fusion i. Heat energy required to complete process of converting unit mass of substance from solid to liquid state without change of temperature is called the Latent Heat of Fusion. • Liquid to Gas – Vaporisation i. Heat energy required to vaporise a unit mass of liquid without temperature rise is called Latent Heat of Vaporisation. • Gas to Liquid – Condensation i. Heat energy expelled is called the Latent Heat of Condensation. • Liquid to Solid – Solidification i. Loss of molecular energy is the Latent Heat of Solidification.
  • 20. • Sublimation i. Some solid substance when heated do not melt, but form a Vapour. ii. Solid to vapour, without passing through liquid state. iii. Eg. Dry ice • Evaporation i. Liquid change to vapour. ii. Some liquid have low boiling point, so easily change from liquid to vapour. iii. Eg. Methylated spirits.
  • 21. Mechanics : statics ; - forces centre of gravity stress and strain properties of matter pressure and buoyancy in liquids
  • 22. Newton’s law of motions First Law of Motion A body at rest will remain at rest unless given an external force, or a body which is moving will keep on moving unless given an external force. ( Inertia ) Second Law of Motion A force proportional to the rate of change of its velocity is produced whenever a body ( or mass ) is accelerated. F = ma Third Law of Motion For every action, there is an equal and opposite direction.
  • 23. MECHANICS STATIC Forces • If a Force is applied to a body it will cause that body to move in the direction of the applied force. • force has both magnitude (size) and direction. • Forces cannot be directly observed, only their effects can be seen.  Compressive - force applied on an object to squeeze it.  Tensile - pair of forces try to extend an object.  Shear - Pair of forces tries to cause one face of material to slide relative to an adjacent face. • Statics is used to describe study of bodies at rest when forces are balanced.
  • 24.
  • 25. • External force – force applied to an object from outside its boundaries. • Internal force – force induced in the object to react against externally applied force. ( Reaction ) VECTOR AND SCALAR • Scalar – just a magnitude, there is no direction associated. eg. Time , mass, volume. • Vector – require both magnitude and direction to be fully defined. eg. Force, velocity, acceleration.
  • 26. Adding Forces • 2 or more forces act at same line, produce resultant force. • If at straight line, subtract or addition. • Forces do not act in a straight line – use the ‘parallelogram law’.
  • 27. Worked example Find the resultant of two forces of 4.0 N and 5.0 N acting at an angle of 45 degree to each other. Using a scale of 1.0 cm = 1.0 N, draw parallelogram ABCD with AB = 5.0 cm, AC = 4.0 N and angle CAB = 45 degree, see figure 8.
  • 28. Worked example: three forces acting on a mass. First resolve each force into its vertical and horizontal components.
  • 29. MOMENTS AND COUPLES • If a body free to rotate about some point ; i. Applied force will cause rotation ii. Force required dependent on how far from hinge force is applied. iii. Turning effect = magnitude and distance. Moment = force x distance. • In SI units, Newtons metres = Newton x metres
  • 30. The Principle of Moments ‘If a body is at rest under the action of several forces, the sum of the clockwise moments about any axis is equal to the sum of the anti clockwise moments about the same axis.’ Type 1 – beam balances where arms are of equal length. Type 2 – lever arrangement can best be seen in design of a wheelbarrow. Type 3 – large effort moves through small distance to overcome small load, which moves through a large distance.
  • 31. • IN EQUILIBRIUM • COUPLE – WHEN TWO EQUAL BUT OPPOSITE DIRECTION, CAUSES ROTATION
  • 32. For example, suppose it is necessary to calculate the resultant moment of a pivot acting on a bell crank lever, refer to diagram below. AO = 100 mm OC = 20 mm BC = 20 mm
  • 33. WHAT IS CENTER OF GRAVITY ?
  • 34. CENTRE OF GRAVITY • Gravity is a force which is always present and is a pulling force in the direction of the center of the earth. • This force acts on every body through an imaginary point called the center of gravity (C of G). • A point where all the weight of a body appears to be concentrated. (total weight can be considered to act through that datum position )
  • 35. (total weight can be considered to act through that datum position )
  • 36. There must be a datum point, such as where when moment in clockwise direction will be balanced by moment in anti-clockwise direction, if given the same amount of force.
  • 37.
  • 38. Stability / balancing • The lower the C of G, the stable an object is. • The wider the base, the more stable an object is – C of G towards the base.
  • 39.
  • 40. • The location of the center of gravity in the human body varies slightly, depending on body shape. • a male with a muscular upper body and small hips, the center of gravity is higher than in a female with narrow shoulders and wide hips • in an infant with a large head in relation to its body, it is higher than in an adult
  • 41. • When force applied to C of G, the body will not rotate. • But if the force is applied offset of the C of G, the body will rotate, or torque will produced.
  • 42. Expressed as an algebraic formula, W1 X1 + W2 X2 + W3 X3 = (W1 + W2 + W3) x G Where G is the position of the centroid, with respect to the datum. G=
  • 43. C of g of an aircraft
  • 44. Why do we need to know c of g of an aircraft ? • To ensure the aircraft is safe to fly, the center-of-gravity must fall within specified limits established by the manufacturer. • C of G range – C of G limits are specified longitudinal (forward and aft) and/or lateral (left and right) limits within which the aircraft's center of gravity must be located during flight. • To evenly load the aircraft – equipments, passengers, baggage, cargo, fuel, etc. • So that C of G range will not be exceeded – prevent aircraft unstable during flight. • Also affects C of G in flight – fuel usage, passengers’ movement, etc.
  • 45. Similar to aircraft, force applied will be acted through the C of G, resulting in torque. Aircraft rotate about its C of G.
  • 46. WHAT IS STRESS ? AND WHAT IS STRAIN ?
  • 47.
  • 48. Stress • If force is exerted on a body, there will be mechanical pressure acting on the body which is called the stress. • A body with having twice the size of other body subjected to a force, it will be stronger and less likely to fail due to applied the applied force. • So, stress is said : Stress = *units : Newton metre -2 , Nm-2 • Components will fail due to over-stressed, not over-loaded.
  • 49. Eg. A tennis ball sealed from atmospheric pressure. So, as long as the external forces acting on it does not exceed the internal forces, the ball will maintain its shape.
  • 50. Forces applied to the body will cause distortion of the body and change to the material’s cross-sectional area ; eg. Tensile Forces will cause elongation . Compressive Force will cause reduction in dimension. • Most material have elastic properties ( it will to return to its original shape after the force is removed ) - provided forces does not exceed limit of elasticity. • There are 5 types of stress in mechanical bodies : i. Tension ii. Compression iii. Torsion iv. Bending v. Shear
  • 51. Tension • force that tends to pull an object apart Compression • resistance to an external force that tries to push an object together.
  • 52. Torsion • Torsional stress is applied to a material when it is twisted. • Torsion is actually a combination of both tension and compression Bending • In flight, the force of lift tries to bend an aircraft's wing upward.
  • 53. Shear • combines tension and compression is the shear stress, which tries to slide an object apart.
  • 54.
  • 55. Strain • If the outside force is great enough to cause the object to change its shape or size, the object is not only under stress, but is also strained. • If a length of elastic is pulled, it stretches. If the pull is increases, it stretches more; if the pull is reduced, it contracts. Hooke’s law states that the amount of stretch (elongation) is proportional to the applied force.
  • 56. How stress varies with stress when a steel wire is stretched until it breaks. Hooke’s Law states that, ‘the amount of stretch (elongation) is proportional to the applied force.’ • Strain - the degree of distortion then has to be the actual distortion divided by the original length (in other words, elongation per unit length). • Strain = change in dimension / original dimension ( No units )
  • 57.
  • 58. *for shearing and torsional stresses, they are expressed as ‘shearing action’ – when one layer of materials move relative to another in direction of applied force. Shear strain – straight motion. Torsion strain – rotational motion.
  • 60. Shear strain Torsion strain • when the applied load causes • form of shear stress resulting one 'layer' of material to move from a twisting action. relative to the adjacent layers. • Twist will be proportional to the applied torque.
  • 62. Properties of matter Diffusion • Is the spreading of a substance of its accord. • due to molecular action, e.g. a smell, whether pleasant or not, travels quickly from its source to your nostrils where it is detected. • occurs in liquids and gases but not in solids.
  • 63.
  • 64.
  • 65. Surface Tension • This suggests that the surface of a liquid behaves as if it is covered with an elastic skin that is trying to shrink. • The surface tension can be reduced if the liquid is ‘contaminated’, adding a detergent to the water will cause our needle to sink. • In a liquid, the molecules still partially bond together and prevents liquid from spreading nag expanding out.
  • 66.
  • 67. Adhesion Force of attraction between molecules of different substances. Cohesion Force of attraction between molecules of same substances.
  • 68.
  • 69. capillary • If a glass tube of small bore is dipped into water , the water rises u the tube a few centimetres. • The adhesion between the glass and the water exceeds the cohesion of the water molecules, the meniscus curves up , and the surface tension causes the water to rise.
  • 70.
  • 71.
  • 72.
  • 73. Mechanical properties of Strength matter A strong material requires a strong force to break it Stiffness A stiff material resists forces which try to change it’s shape or size. Elasticity The ability to recover to its original shape and size after the force deforming it has been reformed. Ductility Materials that can be rolled into sheets, drawn into wires or worked into other useful shapes, without breaking are ductile. Brittleness A material that is fragile and breaks easily .
  • 74. Pressure and buoyancy in • liquid The equivalent term associated with fluids is pressure: pressure = force / area or p = F/A. • Pressure is the internal reaction or resistance to that external force. • Pascal’s Law : “pressure acts equally and in all directions throughout that fluid.”
  • 75. pressure can be transmitted to some other point in order to generate another force.
  • 76.
  • 77.
  • 78. Units of pressure SI system pressure : Pascal = force per unit area ( Nm-2) Atmospheric pressure : Milibars ( mb ) or pounds per square inch ( psi ) Sea level standard atm presssure : 1013-2 mb or 14.69 psi ( at 0C)
  • 79. buoyancy Archimedes’ Principle states that when an object is submerged in a liquid, the object displaces a volume of liquid equal to its volume and is supported by a force equal to the weight of the liquid displaced. THE BUOYANCY OF A SUBMERGED BODY = WEIGHT OF DISPLACED LIQUID – WEIGHT OF THE BODY 1. The body will float--if the buoyancy is positive 2.The body will sink--if the buoyancy is negative 3.The body will be stuck--if the buoyancy is neutral
  • 80.
  • 81.
  • 83. Linear motion • Is the uniform motion in a straight line. • Motion is the change of position of a body with reference to another body. eg. A person sitting in a moving car and passes a building. The person is considered to be at a state of rest in reference to the car. The car is considered to be in motion in relation to the building.
  • 84. speed • Speed tells us how quickly an object is moving at any given point in time. • Scalar quantity – does not take into account the direction of the object travelled. • Average speed – dividing the distance travelled by the time taken. Speed = rate of change of displacement or position = v = where v represents speed.
  • 85. Worked example • An aircraft flies at 80 km/ hr for 15 minutes and at 120 km/hr for a further 15 minutes. How far has it travelled and what is the average speed ?
  • 86. velocity • Includes direction, distance in straight line and time. • Vector quantity – magnitude + distance. eg. An aircraft moves 200miles South West from A to B in one hour. *the velocity is 200mph South West.
  • 87. acceleration • Is the rate of change of velocity over time. • If the rate of change is constant, acceleration is described as being uniform. • Acceleration - If the velocity of an object increases over time. • Deceleration / retardation – If the velocity decreases over time. • If a car is travelling at initial constant velocity ‘u’ and then accelerated with uniform acceleration ‘a’ to final velocity ‘v’, therefore : a = (v–u)/t v = u + at *Unit : m / s 2
  • 88. Equation of linear motion Equations of linear motion V = u + at s=½(u+v)t s = ut + ½at2 v2 = u2 + 2as Free falling objects • if a stationary object is released and free falls under attraction of the force of gravity, it will accelerate at 9.81 m/s 2 • So the ‘a’ will be 9.81 m/s 2 , but in this case it is given the symbol ‘g’. • If the object is thrown upwards, its g will be – 9.81m/s2
  • 89. Initial velocity of objects freefalling from rest is zero, so the equations for free fall are : V = gt S = ½ gt2 V2 = (2gs)2
  • 90.
  • 91. ROTATIONAL MOTION Circular Motion • Rotational motion means motion involving curved paths and therefore change of direction. • Only cases of constant acceleration are considered here. • They are equivalent to those linear equations of motion :
  • 92. Centripetal Force • Continuous force applied to a body moving in circular path to keep it in that particular circular path, preventing it from travelling in straight line ( tangential to circle it is rotating in ) – due to the inertia of the object. • Basically a force acting inwards toward the centre of the circle. • Is directly proportional to the mass of the object in circular motion. • Is inversely proportional to the radius of the circle in which the object travels.
  • 93. Force = ma, so we can say that the object has an inwards acceleration called Centripetal Acceleration which is ; a = v2 , so F = r *where v is linear velocity and r is radius of circular path.
  • 94. Centrifugal Force • Is the equal but opposite reaction to the Centripetal Force. ( Newton’s 3rd Law ) • Tensile Force at the other end of the string acts outwards of the circle.
  • 95. Relationship between Angular and Linear Motion : Providing that we know the value of the rotating body’s radius ( r ), we can use the relationship between the radius and the radian to convert angular values to linear values and vice versa. Linear distance : rθ Linear velocity : rω Linear acceleration : rα
  • 96. Periodic motion • Some masses move from one point to another, then back to the original point, and continue to do this repetitively. • The time during which the mass moved away from, and then returned to its original position is known as the time period, and the motion is known as periodic motion. • Example : pendulum
  • 97. Pendulum • When the mass then displaced from its rest position, it will accelerate back towards its rest position. • On reaching it however, it will not stop, because its inertia carries it on to an equal but opposite displacement. • the time period can be measured from a any position, through to the next time that position is reached, with the motion in the original direction.
  • 98. Cycle –for one complete to and fro movement. Periodic Time – time taken to complete 1 cycle. Frequency – the number of cycle occurring in 1 seconds. ( Hertz – HZ ) Amplitude – maximum displacement of a body from its middle or rest position.
  • 99. Periodic time, T can be calculated by ; T = 2 √ ( L / g ) Where ; L – length of the pendulum g – magnitude of acceleration due to gravity = 9.81 m/s2 For time period ( T ) and frequency ( f ) ; T=1/f , f=1/T
  • 100. Spring – mass systems • If the mass at the spring is displaced and the force is released, the spring force will cause the mass to return to its original position. • It will behave like pendulum, so it continue to move up and down before it stops completely. • Springs obey Hooke’s Law. • The resulting motion, up and down, resulting in :
  • 101. Spring Force Force ( F ) = mg = kE if mg = kE, then the spring constant k = mg E Also, extension E = mg k Frequency (f) = ( 1 / 2 ) √ ( k/m ) where; F is force. m is suspended mass. g is the acceleration due to gravity. E is the spring extension. k is the spring constant.
  • 102. Simple theory of vibration, • harmonics and resonance. but strict law. Analysis of oscillating systems will show that they often obey simple • Acceleration is proportional to the displacement from the neutral position, and in the opposite sense to the direction of the velocity. • Referred to as Simple Harmonic Motion, when acceleration is directed towards fixed point in its path and is proportional to its displacement from that point.
  • 103. Vibration theory • Vibration Theory is based on the detailed analysis of vibrations and is essentially mathematical, relying heavily on trigonometry and calculus, involving sinusoidal functions and differential equations. • Damped vibrations :  Simple pendulum / spring mass will vibrate at constant frequency and amplitude, once it is started.  But vibrations will die away due to other motions such as friction, air resistance, etc.
  • 104. Resonance • When force subjected to force vibration, it will vibrate along with natural frequency of the object. • If the natural frequency matches the resonant frequency with forced vibration causes the amplitude to increase dramatically. • Natural frequency tries to damped out the amplitude but cannot damp its own natural frequency. • So the two amplitudes combine to produce resonance.
  • 105. Velocity ratio, mechanical advantage and efficiency. • Machine – utilise some form of motion to convert an applied force into a useful work output • The input forces is often amplified many times by the machine so that we can overcome a heavy load with little effort. • Eg ; levers, pulleys, gears, screws. Velocity ratio • Ratio of distance the effort is required to move in comparison with the distance the load moves in the same time. Velocity Ratio = Distance moved by effort Distance moved by load
  • 106. Mechanical Advantage • Describes the ratio of load moved with the effort required to move it. Mechanical Advantage = Load Effort *A rusty car jack will have a low mechanical advantage because much of the effort would be used to overcome the friction of a corroded screw thread. Efficiency • Describes the ratio of the useful work done by a machine to the total work put into it. Efficiency = Work Output x 100% or Mechanical Advantage x100% Work Input Velocity Ratio • Expressed as percentage and is always less than 100%. *Friction and slippage can detract from efficiency of a machine.
  • 107. LEVERS • Used to gain mechanical advantage. • Most basic form : seesaw that has weight at each end. ( weight on one end tends to rotate it clockwise, weight on the other end tends to rotate it anti-clockwise ) First Class Lever • Lever has fulcrum between load and effort. • Less effort required to lift the load.
  • 108. Second Class Lever • Has fulcrum at one end of the lever and effort is applied to the opposite force. Third Class Lever • Force is applied between fulcrum and load. • Used to move the load a greater distance than effort applied. • Disadvantages : much greater effort required to produce moment.
  • 109. Pulleys • Pulley wheel has circumferential groove to accept a rope. • Effort is applied by pulling on a rope. • Tension created in the rope and movement are transmitted through arrangement to the load. • Single fixed pulley is a convenient means of lifting a light load. • So, for instance, if one end of the rope is attached to a fixed object, pulling on the other end will apply a doubled force to any object attached to the axle.
  • 111. Mass • Is the quantity of matter that it contains. • Constant regardless of its location. • Basic SI unit : kilogram (kg) • Imperial : pounds (lbs) Weight • Force with which gravity attracts a body. • Varies with distance between body and centre of the earth, so if farther than centre of the earth, the less it weighs. • So, it is said that an object in deep space does not has no weight, but do has mass. • Gravitational acceleration is considered as 9.81m/s2 Force • Is a vector quantity that has magnitude, direction and a point of application. • Which changes a body’s state of rest or of uniform motion.
  • 112. Inertia • Newton’s First Law • A body at rest will stay at rest unless given an external force, or a moving body will continue on moving unless given and external force. • Is the resistance to movement or changes. Work • Work is done when a force move. Work done = force x distance moved in the direction of the force. • Unit : Newton metre (Nm) or the joule 1 joule = the work done when a force of 1 Newton is applied through a distance of 1 metre
  • 113. Power • The amount of work done in specific time. Power = work done = force x distance time taken time • Si unit : Watt ( W ) – 1 Joule/ second • Is the rate of work done when 1 Joule is achieved in one second. *One horsepower is the equivalent of 746 Watts Brake Horse Power • To rate the engine power. • The engine is made to do work on a device known as dynamometer or ‘brake’ – loads the engine output. Shaft Horse Power • Measure output shaft of a turboprop engine, since the power produced at shaft is what will be delivered to propeller.
  • 114. Energy • Is the capacity to do work. • Si unit : Joules • Can appear as several form ; mechanical, chemical, heat, electrical, and radiation. • But only deal with Mechanical Energy, and appears as potential and kinetic energy. • Energy cannot be created or destroyed, it can only be changed from one form to another. • Energy will not be converted into 100% work, they will always appear in a less useful form such as wasted heat. • But it may be converted into 100% energy.
  • 115. Potential Energy (PE) • Energy is possesses by virtue of its position or state. • Example : A mass raised to a height above the ground has potential energy since its weight is capable of doing work as it descends to the ground under the influence of gravity. Work = force x distance *since PE is for mass at elevated position,so distance is the height above ground. Potential Energy = mass x gravity x height = mgh
  • 116. Kinetic Energy • Energy it possesses by virtue of its motion. • Arises from the work done on it. • When body set in motion by a force doing work it acquires kinetic energy, which will work against any forces that try to resist it. Kinetic Energy = ½ mv2
  • 117.
  • 118. Conservation of Energy “ Whenever energy is converted from one form to another, none of it is lost.” • The sum of the energy can always be accounted for in the other forms of energy that may have converted into. • After an object hits ground on a fall, the energy has converted into heat energy and will be dissipated into the air. • So a comparison between work out and work in is obviously a measure of the system efficiency. Efficiency = work output work input *usually expressed as percentage ( less than 100 % ).
  • 119. Heat • Defined as energy between two bodies because of difference in temperature. • If two bodies at different temperature, are bought into contact, their temperature become equal. • Energy that flows from a hot place to a cooler place. • Heat energy can be transferred by ; conduction, convection and radiation.
  • 120. momentum • Product of its mass and velocity. momentum = mass x velocity • SI unit ; kgm/s Impulse of a force • If a body was subjected to a sudden blow, shock load or impact, it will be possible to measure change in momentum. • Forces which have the short time duration are called the Impulsive forces. • Change of momentum due to impulsive force is called the Impulse. • Impact duration small – impulsive force large. Impact duration large – impulsive force small.
  • 121. Impulse • Product of force and time or change in momentum. • For example, if we rest the hammer, on top of the head of a nail, neither the hammer nor the nail has any momentum. • However, if we bring the hammer down from a height and strike the nail sharply on its head, both the hammer and nail will move after the impact. In a short time they will come to rest with the nail having penetrated whatever it is under it. • Impulse = change in momentum = mass x change in velocity. = force ( N ) x time ( seconds )
  • 122. CONSERVATION OF MOMENTUM “When two or more masses act on each other, the total momentum of the masses remains constant, provided no external forces, such as friction, act.”
  • 123. CONSERVATION OF MOMENTUM MOTION MOMENTUM First law First Law Mass remains at rest or continue to Mass remains at rest or continue to move at constant velocity, unless acted move at constant velocity, unless acted on by an external force. on by an external force. Second Law Second Law F = ma Rate of change of momentum is proportional to the applied force. Third Law Third Law For every action, there is a n equal and If mass A exerts force on B, then B exerts opposite reaction. an equal but opposite force on A.
  • 124. Changes in Momentum Change of Momentum = final momentum - initial momentum = ( mv) - (mu) Rate of change of momentum = change in momentum time taken = mv–mu t *The rate of change of momentum is proportional to magnitude of force causing it. • When two bodies, one of low mass and the other of high mass, are acted upon by the same force for the same time, the low body mass will build up higher velocity than the heavy mass.
  • 125.
  • 126. For example; At (a) – mass A overtakes mass B. At (b) – mass B will be accelerated by impulsive force delivered by mass A, and mass A will be decelerated by an impulsive force delivered by B . At (c) – after the impact, mass A and B will have new velocities Va and Vb. Momentum before impact equals to momentum after impact.
  • 127. Example : A moving snooker balls, each ball has its own momentum before collision. After collision, the sum of the two balls’ momentum will be the same as the sum prior to the collision even though their velocities may have changed. sum of momentums of balls = sum of momentum after impact prior to impact mu1 + mu2 = mv1 + mv2
  • 128.
  • 129. Moment of inertia • considers the effect of mass on bodies whose moment is rotational. • Moment of inertia is a function of mass and radius. • Consider the two cylinders, of equal mass, but different dimensions, capable of being rotated. • The LH cylinder is easier to rotate than RH cylinder.
  • 130. GYROSCOPES • is a rotor having freedom of motion in one or more planes at right angles to the plane of rotation. • used in several of an aircraft’s instruments, which are vital to the safety of the aircraft in bad weather. • For example wheels, engines, propellers, electric motors and many other components must run with perfect smoothness.
  • 131. With the rotor spinning, the gyroscope will possess two fundamental properties: Gyroscopic rigidity or inertia Gyroscopic precession
  • 132. Gyroscopic rigidity • maintains the axis of rotation constant in space. • if a gyroscope is spinning in free space and is not acted upon by any outside influence or force, it will remain fixed in one position. • The degree to which the rotor offers resistance depends on 3 things :  Mass of the rotor – greater the mass, greater resistance to change in direction of plane of rotation.  Angular speed of the rotor – higher the speed, greater the resistance.  Radius of gyration of the rotor – bigger the radius, greater the rigidity.
  • 133. Gyroscopic Precession • angular change of direction of the plane of rotation of a gyroscope, as a result of an external force. • The rate of this change can be used to give indications such as the turning rate of an aircraft.
  • 134. I. The rotor will rotate about axis AA. II. Apply a force so that it acts on the rim of the rotor at 900. III. Move this force around the rim of the rotor so that it moves through 900 and in the same direction as the rotor spins. IV. Precession will move the rotor in the direction that will result in the axes of applied force and of rotation coinciding. V. For a constant gyroscopic speed, the rate of precession is proportional to the applied force. VI. The opposite also applies, so for a given force the rate of precession is inversely proportional to rotor speed.
  • 135.
  • 137. Determining Precession Direction • If a mass is mounted on a rotating shaft, and the centroid is offset from the axis of rotation, mass will exert centrifugal force on the shaft. • Even if the eccentricity is small, force may be considerable at high speed. • So, it will cause the shaft to bend. • If large stresses produced, will cause damage to bearing. • Addition by vibrations from supports and surroundings will cause undesirable effect. • Some eccentricity is due to manufacturing imperfections or design, so it is unavoidable. • Balancing is needed to eliminate effect of centrifugal force. • Eg ; weights put on car wheels to balance them, make it easier to drive at high speed.
  • 138. Friction • Force that resists any sliding movement between two contacting surfaces. • Can be taken as advantage, for brakes on vehicle to try to walk on smooth surface. • Frictional force depends on nature between two surfaces. • Acts in any directions but always acts in opposing motion.
  • 139. angle of the plane (θ) is increased, the body remains stationary, until at some particular value of θ, it begins to move down the plane. • At this maximum value, the force opposing motion Fmax = mg sin θ , • and the normal reaction between the body and the plane R = mg cos θ. F/ R = mg sin θ / mg cos θ = tan θ • ratio F/R (tan θ) is termed the Coefficient of Friction ( μ ) - < 1. μ = F = tan θ R
  • 140. Coefficient of Static Friction • Static friction is friction between two solid objects that are not moving relative to each other. • The static friction force must be overcome by an applied force before an object can move. • The maximum possible friction force between two surfaces before sliding begins is the product of the coefficient of static friction. • sometimes referred to as limiting friction. • Coefficient of Static Friction (μ) = Friction Force ( F ) Normal Reaction ( N ) • Frictional Force , F = μN
  • 141. Coefficient of Dynamic Friction • Dynamic friction is when two objects are moving relative to each other and rub together (like a sled on the ground). • The amount of force required to keep the object moving is called the coefficient of dynamic friction. • usually less than the coefficient of static friction for the same materials
  • 142. There are several types of friction: • Dry friction resists relative lateral motion of two solid surfaces in contact. Dry friction is subdivided into static friction between non-moving surfaces, and kinetic friction between moving surfaces. • Fluid friction describes the friction between layers within a viscous fluid that are moving relative to each other. • Lubricated friction is a case of fluid friction where a fluid separates two solid surfaces. • Skin friction is a component of drag, the force resisting the motion of a solid body through a fluid. • Internal friction is the force resisting motion between the elements making up a solid material while it undergoes deformation.
  • 144. Fluid – term used for liquid and gases. Specific gravity and density • Density – mass per unit volume. • Varies with : Temperature ( for solids and liquid ) Temperature and pressure ( gas ) Density ( ρ ) = mass volume • Eg : liquid that fills a certain container has a mass of 756 kg. The container is 1.6 m long, 1.0 m wide and 0.75 of a metre deep. The liquid density should be ? ρ = 756 = 630kgm-3 1.2
  • 145. Standard conditions for the measurement of gas density is established at 00C and a pressure of 1013.25 milli-bars (Standard atmospheric pressure). • Temperature change will not change the mass of the substance, but as temperature change, the substance tend to expand or contract, altering the volume.
  • 146. Relative Density • It is necessary to compare density of one substance with the other to achieve a standard which all other substance can be compared. • For solid and liquid, compare with water at 40C. • For gas, compare with air. Relative Density = mass of any volume of a substance mass of equal volume of water / air • Eg ; if a hydraulic fluid has relative density of 0.8, then 1L of the liquid wieghs 0.8 times as much as 1L of water.
  • 147. Hydrometer • Used to measure the relative density of liquids. • Glass float contained within cylindrical glass body. • Weight at the bottom, scale at the top. • When liquid drawn into the body, float displays relative density on graduated scale. • Immersion in pure water will give out reading of 1.000. • App. in aviation : to measure battery electrolyte and fuel.
  • 148. Viscosity • Measure of the resistance of a fluid which is being deformed by either shear stress or tensile stress. • Also known as "thickness" or "internal friction“. • Eg : water has ‘thin’ velocity, while honey has ‘thick’ velocity. • so there is friction between two liquid surfaces even when they consist of the same liquid. • This internal friction opposes the motion of one layer over another and, when it is great, it makes the flow of the liquid very slow. • Viscosity of a liquid rapidly decreases as its temperature rises.
  • 149. Viscosity of different liquids can be compared in different ways. • Eg ; if we allow fluids of different viscosity run out of container, the higher the viscosity, the longer time taken to empty the container. • It is important to know about viscosity as aircraft uses fluids such as oil in the engine for lubrication.
  • 150. Fluid Resistance Skin friction • Resistance present on a thin, flat plate which is edgewise on to a fluid flow. • Near the surface, the fluid is slowed up due to roughness of the skin, and fluid can also be considered as stationary at the surface. • Effected by skin smoothness. • The rougher the skin, the higher the friction.
  • 151. Eddies or turbulent airflow • swirling of a fluid and the reverse current created when the fluid flows past an obstacle. • The moving fluid creates a space devoid of downstream-flowing fluid on the downstream side of the object. • Eg. If you put plate at right angles to flow, turbulence will be created behind the plate and a very high resistance .
  • 152. Effect of streamlining • flowing steadily over a smooth surface, narrow layers of it follow smooth paths that are known as streamlines. • This smooth flow is also known as laminar flow. • If laminar flow encounter obstructions, the streamline will break and become irregular or turbulent. If fluid flows slowly along pipe, the flow is streamline. If flow is very fast and exceeds a certain critical speed, the flow will become turbulent.
  • 153.
  • 154. The Compressibility of Fluids • All fluids are compressible, so that their density will change with pressure. • Fluid ; i. assume as incompressible – provided under steady flow conditions, and changes of density small. • Gases ; i. easily compressed – except when changes of pressure and density are small.
  • 155. Static and Dynamic Pressure • Pressure acting on x x1 is due to the weight of the fluid acting downwards. • W = mg ( g = gravitational force ) mass = volume x density = height x cross-sectional area x density = hAρ so, downwards force = h . ρ . g . A acting on A and pressure will be = h ρ g . A A =hρg
  • 156. Static pressure • Act depth h, within a stationary fluid of density ρ. • Reduces density accompanied by reduced pressure. Dynamic pressure • Eg, moving air is essential in flight. • Dynamic presssure = ½ ρv2 where ρ = density, v = velocity.
  • 157. Worked example What is the pressure at 10.5 m deep of liquid in a pool having the density of 2.5kg/m3 ? What is the depth of an object from the surface if pressure exerted on it is 100psi in a 5.3kg/m3 liquid ?
  • 158. Bernoulli’s Theorem • a principle that explains the relationship between potential and kinetic energy in a fluid. • In a fluid the potential energy is that caused by the pressure of the fluid, while the kinetic energy is that caused by the fluid’s movement. • As a fluid enters a venturi tube, it is travelling at a known velocity and pressure. • When the fluid enters the restriction it must speed up, or increase its kinetic energy. However, when the kinetic energy increases, the potential energy decreases and therefore the pressure decreases.
  • 159.
  • 160.
  • 161.
  • 163. Laws Of Thermodynamics First Law Energy cannot be created or destroyed. It can only be converted from one to another. When the energy converts from one form into other forms the total quantity of energy remains the same. Second Law Heat can only transfer from a high temperature region to a lower temperature region. It cannot naturally transfer the other way. Third Law The transfer of energy from matter becomes increasingly difficult as its temperature approaches absolute zero. It is considered impossible at absolute zero.
  • 164. Temperature • Heat is a form of energy that causes molecular agitation within a material. • is a measure of the kinetic energy of molecules. • Temperature scale; Freezing – 00C Boiling – 1000C • Farenheit Scale - when you increased the temperature of a gas by one degree Celsius, it expands by 1/273 of its original volume. • So if the temperature was decreased to 273 degrees below zero, the volume of the gas would also decrease to zero, and there would be no more molecular activity – absolute zero. • On the Celsius scale absolute zero is - 2730C. On the Fahrenheit scale it is – 4600F. • Conversion ; – °C x 9/5 + 32 = °F ( from Deg. Centigrade to Farenheit ) – (°F - 32) x 5/9 = °C ( from Farenheit to Deg. Centigrade )
  • 165.
  • 166. Heat • is the exchange of thermal energy from a hot body to a cold body. • When a hot body and a cold body have contact, heat will flow from the hot body to the cold body until they both reach thermal equilibrium (they are at the same temperature). • For example ; When an aircraft’s brakes are applied, the kinetic energy of the moving aircraft is changed into heat energy by the rubbing action of the brake friction material against the brake discs. • SI system : Joule (J) British thermal unit (Btu) calorie (cal) Heat & Work Conversion Factors 1J 0.2388 cal 1 cal 4.1868 J 1 Btu 1055 J 1J 0.000 947 Btu 1 Btu 0.252 cal 1 cal 3.968
  • 167. Heat Capacity • specific heat - amount of heat per unit mass required to raise the temperature by one degree Celsius. • Relationship between heat and temperature change : Q = cmΔT Q is the heat added in 0C C the specific heat capacity in J / kg0C M is the mass in kg ΔT is Tfinal – Tinitial in 0C
  • 168. Different materials require differing amounts of heat energy to change their temperature. • The heat energy required to change the temperature of 1 kg of material by 1 K is known as the specific heat capacity (c) of the material. • Due to the high specific heat of water, oceans and large lakes serve as temperature stabilisers. • Land surfaces have a much lower specific heat, and the temperature can vary significantly throughout the day.
  • 169. Heat Transfer • three methods by which heat is transferred from one location to another or from one substance to another, which are : conduction convection radiation
  • 170. Conduction • When body having high heat energy in contact with body having low heat energy. • Eg; When hot object in contact with cold object, energy of molecules from hot object will be transferred to molecules of cold object until they have the same amount of energy ( stabilize ). • Various metals have different rates of conduction. • Liquids are poor conductors of heat in comparison with metals. • .Gases are even worse conductors of heat than liquids. • Insulators are materials that reduce or prevent heat conduction.
  • 171. Convection • process by which heat is transferred by the movement of a heated fluid. • Transfer of heat by convection is often hastened by the use of a ventilating fan to move the air surrounding a hot object. • Eg ; when heat is absorbed by a free-moving fluid, the fluid closest to the heat source expands and its density decreases.
  • 172. Radiation • is the only form of energy transfer that does not require the presence of matter. • refers to the continual emission of energy from the surface of all bodies. • This energy is known as radiant energy of which sunlight is a form. • This is why you feel warm standing in front of a window whilst it is very cold outside . Expansion and Contraction • All materials expand and contract with a change in temperature. gases which expand the greatest amount . Solids and liquids expand much less than gases
  • 173.
  • 174.
  • 175. Volumetric Expansion • Expansion – considered as change in length, change in area or change in volume. • Different materials expand at different rates. Expansion of Solids • Expansion is proportional to the increase in temperature to the original dimension and depends on the actual material used. L2 - L1 = L1 (θ2 - θ1)α L2 and L1 are final and initial lengths, θ2 and θ1 are final and initial temperatures α is a material constant (coefficient of linear expansion).
  • 176. Expansion of Fluids • Fluids expand more than solids. • For gases, as volume and temperature changes are usually accompanied by pressure changes.
  • 177. The law of Thermodynamics • Thermodynamics is the study of the way that one does work with heat. • Energy conservation limits the amount of work we can get out of a certain amount of heat.
  • 178. first law of thermodynamics • States that energy is conserved. • The change in internal energy of a system is equal to the heat added to the system minus the work done by the system. ΔU = Q – W (Δ is the mathematical symbol for a change in a quantity) ΔU is the change in internal energy, Q is the heat added to the system W is the work done by the system. • ΔQ is positive if it is put into the system, negative if it is taken out of the system. • ΔW is positive if the system does work on its surroundings and is negative if work is done on the system. • The internal energy is the sum of the kinetic and potential energy of the atom and molecules that make up the system.
  • 179. second law of thermodynamics • general principle which places constraints upon the direction of heat transfer and the attainable efficiencies of heat engines. • States that heat transfer will occur naturally of its own accord down the temperature gradient. • Heat will naturally flow from a hot region to a cool region but not the other way around.
  • 180. the basic sense of the principle : Heat will not flow spontaneously from a cold object to a hot object. You cannot create a heat engine which extracts heat and converts it all to useful work. There is a thermal bottleneck which constrains devices which convert stored energy to heat and then use the heat to accomplish work.
  • 181. gases • Ideal gas - one in which all collisions between atoms or molecules are perfectly elastic and in which there are no intermolecular attractive forces. • a collection of perfectly hard spheres which collide but which otherwise do not interact with each other. • all the internal energy is in the form of kinetic energy and any change in internal energy is accompanied by a change in temperature.
  • 182. From the Ideal Gas Law ; =
  • 183. Boyle’s Law If temperature is constant ; P1V1 = P2V2 Charles’ Law If pressure is constant ; =
  • 184.
  • 185. Isothermal and Adiabatic Processes Isothermal process - in which the temperature in a system remains constant. Adiabatic process - one where no heat is added to, or taken away from the system. Heat engine • heat engine is a system that performs the conversion of heat or thermal energy to mechanical work.
  • 186. Heat Engine Processes • a useful process is the adiabatic process where no heat enters or leaves the system. • The first law of thermodynamics with Q=0, i.e. heat = zero shows that all the change in internal energy is in the form of work done. • internal energy is proportional to temperature, there is no change in the internal energy of the gas during an isothermal process. • All the heat added to the system is used to do work.
  • 188. Carnot Cycle • consisting of two isothermal processes and two adiabatic processes. • can be thought of as the most efficient heat engine cycle allowed by physical laws. • the Carnot efficiency sets the limiting value on the fraction of the heat which can be so used. • In order to approach the Carnot efficiency, the processes involved in the heat engine cycle must be reversible and involve no change in energy available to do work. • This means that the Carnot cycle is an idealisation, since no real engine processes are reversible and all real physical processes involve some increase in energy available to do work .
  • 189. Heat Flow to Hotter Region • internal energy will not spontaneously flow from a hot region to a cold region. • But if external force is given, heat can flow from cold region to hot region. • Usually this is done with the aid of a phase change, i.e., a refrigerant liquid is forced to evaporate and extract energy from the cold area. . Then it is compressed and forced to condense in the hot area, dumping its heat of vaporisation into the hot area.
  • 193. Speed Of Light • is one form of transmission of Electro-magnetic energy. • travels at high speed (about 3 x 108 metres per second) and in straight lines. • Can be ‘bent’ or reflected.
  • 194. Laws Of Reflection and Refraction Reflection • Light can also be reflected. • Observation and measurement will show that ; a. the incident and reflected rays lie in the same plane. b. the angle of incidence equals the angle of reflection.
  • 195. Plain and Curved Mirrors • When you look in a mirror, you see a reflection, usually termed an image. • For example, if an object is viewed from two different angle, the reflected rays : – appear to come from which corresponds to the image. – lies on the same normal to the mirror as the object. – appears the same distance behind the mirror as the object is in front. – Appears as the same size.
  • 196. For mirror that is not plain, it may be curved, spherical and parabolic. • Incidence equals reflection - still holds, but the curved surface allows the rays to be focused or dispersed. FP is known as the focal length. Note the rays actually pass through F, and a real image can be formed. FP is still the focal length, but the image is virtual.
  • 197. The size of the image depends on the position of the object. • image may be smaller or larger. • If the object is near to the mirror, the image will be far and larger from the mirror but in opposite plane. • If the object is far from the mirror, the image will be nearer and small, between the position of object and mirror in opposite plane. magnification = image height object height • For spherical mirror, magnification = image distance object distance
  • 198.
  • 199. Concave mirrors (e.g. shaving mirrors) give a magnified, erect (right way up) image, if viewed from close-to. • Convex mirrors (e.g. driving mirrors) give a smaller, erect image, but with a wide field of view. • Parabolic reflectors can focus a wide parallel beam. By placing the bulb at the focus, they can produce a strong beam of light. (Conversely, they can focus microwave signals when used as an aerial).
  • 200. Refraction • A submerged object is often seen at reduced depth. • This is because the ray has been ‘bent’ at the water / air boundary.
  • 201.
  • 202. Refraction Index • Since the angle of incidence and refraction is not the same ; sine i = μ ( a constant ) sine r • depends on the 2 mediums involved. μ = speed of light in medium 1 speed of light in medium 2
  • 203.
  • 204.
  • 205. Ray (1) has been refracted across the boundary, but ray (2) has been internally reflected at the boundary. critical angle of incidence when the ray in the denser medium does not emerge, but travels along the boundary. • sine C = 1 / μ exists • Refraction is the basic principle which explains the workings of prisms and lenses.
  • 206. Total Internal Refraction • Refraction at a denser medium, a beam of light is bent towards the normal and, vice versa. • APB – ray reflected away. • AP’D – angle of incidence increased, angle of refraction becomes 900 . • AP”C – Angle of incidence further increased , angle of refraction is >900 , remaining in the boundary. • Total internal refraction – where none of lights passing through the boundary.
  • 207.
  • 208.
  • 209. Convex and Concave Lenses • The light rays then meet the surface of the lens at an angle to the normal, and are then refracted. • Images can be real or virtual, erect or inverted, and larger or smaller. • The nature of the image will depend on the type of lens, and the position of the object in relation to the focal length of the lens, (the focal length is a function of the curvature of the lens surfaces).
  • 210.
  • 211.
  • 212.
  • 213.
  • 214.
  • 215.
  • 216. Fibre Optics • Depends upon the total internal reflection of light rays. • Light can be trapped by total internal reflection inside a bent glass rod and piped along a curved path as in the diagram below. a single, very thin glass fiber behaves in the same way. • They are small and so, once light is introduced into the fiber with an angle within the confines of the numerical aperture of the fiber, it will continue to reflect almost losslessly off the walls of the fiber and thus can travel long distances in the fiber. • If a bundle of parallel fibers is used to construct an optical transmission line, images can be transferred from one point to another.
  • 217. Fibre Optic Imaging • Principle : light striking at one end will be transmitted to the other end of the fibre. • If the arrangement of fibres in the bundle is kept constant then the transmitted light forms a mosaic image of the light which struck the end of the bundle.
  • 218. Wave motion and sound
  • 219. Wave motion • For example, wave is created at a lake or pond due to disturbance, such as a rock thrown into the water. • The water wave has a crest and a trough and travels from one location to another. • One crest is often followed by a second crest which is often followed by a third crest, and so on. • waves may be circular waves which originate from the point where the disturbances occur; such circular waves travel across the surface of the water in all directions.
  • 220. Another example, if a slinky is stretched out from end to end, a wave can be introduced into the slinky by either vibrating the first coil up and down vertically or back and forth horizontally. • As the wave moves along the slinky, each individual coil is seen to move out of place and then return to its original position. • The wave does not stop when it reaches the end of the slinky; rather it seems to bounce off the end and head back from where it started.
  • 221. Categories of Waves • Waves come in many shapes and forms. • Some share basic characteristic properties and behaviours, some waves can be distinguished from others based on some very observable (and some non-observable) characteristics. • It is common to categorise waves based on these distinguishing characteristics. Transverse Wave Direction of movement Longitudinal wave Surface Wave To categorize wave Electromagnetic Waves Ability to be transmitted through vacuum Mechanical Waves
  • 222. Direction Of Movement Transverse wave • Wave moves in a direction perpendicular to the direction which the wave moves. • If pulse is applied to the left end by vibrating it up and down, the energy will be transported from left to right and particle will be displaced upwards and downwards.
  • 223. Longitudinal Wave • Wave in which particles of the medium move in a direction parallel to the direction which the wave moves. • If force is applied to the left end by vibrating it left and right, the energy will be transported from left to right and particle will be displaced rightwards and leftwards.
  • 224. Ability to transmit through vacuum Electromagnetic Wave • wave which is capable of transmitting its energy through a vacuum. • Electromagnetic waves are produced by the vibration of electrons within atoms on the Sun's surface. • These waves subsequently travel through the vacuum of outer space, subsequently reaching Earth. • Eg ; Light Wave. Mechanical Wave • Wave which is not capable of transmitting its energy through a vacuum. • Require a medium in order to transport their energy from one location to another. • Eg ; Sound Wave.
  • 225. Anatomy of Waves • dashed line - equilibrium or rest position of the string. (if there were no disturbance moving through it ) • Points A and F - crests of this wave (point on the medium which exhibits the maximum amount of positive or upwards displacement from the rest position) • Points D and I - troughs of this wave (point on the medium which exhibits the maximum amount of negative or downwards displacement from the rest position )
  • 226. Amplitude of a wave - maximum amount of displacement of a particle on the medium from its rest position. ( from rest to crest ) • Wavelength ; a. Simply the length of one complete wave cycle. b. Wave has a repeating pattern. And the length of one such repetition (known as a wave cycle) is the wavelength. c. Can be measured as the distance from crest to crest or from trough to trough. ( B – G, E - J, D – I )
  • 227. Longitudinal wave • is a wave in which the particles of the medium are displaced in a direction parallel to the direction of energy transport. • Wavelength - determined by measuring the distance between any two corresponding points on adjacent waves. ( measure distance from a compression to the next compression or from a rarefaction to the next rarefaction ; A – C , B – D )
  • 228. Frequency and Period of a Wave • Frequency ; a. refers to how often the particles of the medium vibrate when a wave passes through the medium. b. number of complete vibration cycles of a medium per a given amount of time and it as the units of cycles per second or Hertz (Hz) where 1 Hz is equivalent to 1 cycle/second. c. . A detector could be used to detect the frequency of these pressure oscillations over a given period of time. d. unit : Hertz, Hz ( cycle / sec ) • Period ; a. the time which it takes to do something. b. the time for a particle on a medium to make one complete vibration cycle. c. When an event occurs repeatedly, then we say that the event is periodic. d. measured in units of time such as seconds, hours, days or years.
  • 229. Interference Phenomena Wave interference • phenomenon which occurs when two waves meet while travelling along the same medium. • Causes the medium to take on a shape which results from the net effect of the two individual waves upon the particles of the medium. • Eg ; if 2 crests of wave having amplitude of +1 move into each other, the resulting sine crest +2 is created at the moment when the 2 waves overlapped. • Sometimes called Constructive Interference.
  • 230. Constructive Interference • Occurs at any location along the medium where the two interfering waves have a displacement in the same direction. • If both waves have an upward displacement; consequently, the medium has an upward displacement which is greater than the displacement of the two interfering pulses.
  • 231. Destructive Interference • type of interference which occurs at any location along the medium where the two interfering waves have a displacement in the opposite direction. • If a sine crest with an amplitude of +1 unit meets a sine trough with an amplitude of -1 unit, destructive interference occurs. • The two pulses cancel each other for the duration of the overlap. • Once the two pulses pass through each other, there is still a crest and a trough heading in the same direction which they were heading before interference.
  • 232. Principle of Superposition “When two waves interfere, the resulting displacement of the medium at any location is the algebraic sum of the displacements of the individual waves at that same location.” • To determine the shape of the resultant wave caused by the interference of two separate waves. • Standing Wave pattern : An interference phenomena. When the vibration frequency of the source causes reflected waves from one end of the medium to interfere with incident waves from the source in such a manner that specific points along the medium appear to be standing still. Only created within the medium at specific frequencies of vibration; these frequencies are known as harmonic frequencies, or merely harmonics. From the presence of two waves (sometimes more) of the same frequency with different directions of travel within
  • 233. Anti-nodes - point A on the medium moves from a positive to a negative displacement over time. • Nodes - point B on the medium is a point which never moves.
  • 234. Standing Wave • stationary wave - is a wave that remains in a constant position. • often applied to a resonant mode of an extended vibrating object. • created by constructive interference of two waves which travel in opposite directions in the medium, but the visual effect is that of an entire system moving in simple harmonic motion. • modes of vibration associated with resonance in extended objects like strings and air columns have characteristic patterns called standing waves. • arise from the combination of reflection and interference such that the reflected waves interfere constructively with the incident waves. • An important part of the condition for this constructive interference for stretched strings is the fact that the waves change phase upon reflection from a fixed end.
  • 235.
  • 236.
  • 237.
  • 238.
  • 239. Sound • Sound wave - pressure disturbance which travels through a medium by means of particle interaction. • As one particle becomes disturbed, it exerts a force on the next adjacent particle, thus disturbing that particle from rest and transporting the energy through the medium. • speed of a sound wave refers to how fast the disturbance is passed from particle to particle. • frequency refers to the number of vibrations which an individual particle makes per unit of time. • speed refers to the distance which the disturbance travels per unit of time.
  • 240. Speed of Sound • Is determined to be 331 ½ m / s at 00C – 1087 ft /s , 741 mph or 644 kts. • liquids are better transmitters of sound. • Eg. sound waves travel approx. 4 times faster in water than in air and speed of sound in solids is even greater, sound travels through steel is 15 times faster than it travels in air. speed ( sound wave ) = frequency x wavelength • Alteration in wavelength effects the frequency, but not the wave speed. • Doubling of wavelength results in halving the frequency, but wave speed doe not change. • The speed of sound wave depends on the properties of the medium through which it moves.
  • 241. Primarily affected by temperature, the lower the temperature, the lower the speed of sound. speed of sound = √ ( γ R T ) where γ = ratio of specific heats of the gas R = gas constant T = gas temperature ( in Kelvin ) • It determines the nature and formation of shock waves. Mach No = True Airspeed of aircraft Speed Of Sound
  • 242. Intensity • amount of energy which is transported past a given area of the medium per unit of time. • Often referred to as ‘loudness’ , the energy of the wave. • The greater the amplitude of vibrations of the particles of the medium, the greater the rate at which energy is transported through it, and the more intense that the sound wave is. • Intensity is the energy/time/area; and since the energy/time ratio is equivalent to the quantity power, intensity is simply the power/area. Intensity = Energy or Intensity = Power Time x Area Area • Eg ; if amplitude of sound wave is doubled, intensity will increase fourfold. • Unit : Watts / Meter2 . But scale to measure intensity; Desibel (dB)
  • 243. Pitch • Best described as position on musical scale. • The ears of humans (and other animals) are sensitive detectors capable of detecting the fluctuations in air pressure which impinge upon the eardrum. • The human ear is capable of detecting sound waves with a wide range of frequencies, ranging between approximately 20 Hz to 20 000 Hz. • The sensations of these frequencies are commonly referred to as the pitch. • A high pitch sound corresponds to a high frequency and a low pitch sound corresponds to a low frequency.
  • 244. Doppler Effect • effect produced by a moving source of waves in which there is an apparent upward shift in frequency for the observer and the source are approaching and an apparent downward shift in frequency when the observer and the source is receding. • Occur with all types of waves - most notably water waves, sound waves, and light waves.
  • 245. Doppler Effect observed because the distance between the source of sound and the observer is changing. • If the source and the observer are approaching, then the distance is decreasing and if the source and the observer are receding, then the distance is increasing. • If the source is moving towards the observer, the observer perceives sound waves reaching him or her at a more frequent rate (high pitch); and if the source is moving away from the observer, the observer perceives sound waves reaching him or her at a less frequent rate (low pitch).