SlideShare ist ein Scribd-Unternehmen logo
1 von 17
3. Analysis of Trusses
▪ Method of Joints:
• For the forces acting on the connecting pin of each joint,
- First, finding the forces in the members of a truss
consists of satisfying the conditions of equilibrium.
- Therefore, deals with the equilibrium of concurrent
forces,
- And only two independent equilibrium equations are
involved.
3. Analysis of Trusses
▪ Method of Joints:
• Begin the analysis with any joint ,
- Where at least one known load exists
and where not more than two unknown.
• Usually designate the force in each member by the two
letters defining the ends of the member forces are present.
• The solution may be started with the pin at the left end.
3. Analysis of Trusses
▪ Method of Joints:
• Free-body diagram is shown in Fig.

• Portions of members AF and AB are shown to indicate the
mechanism of the action and reaction.
3. Analysis of Trusses
▪ Method of Joints:
• AB makes contact on the left side of the pin.
If we consistently draw the force arrows on the same side of
the pin as the member, then tension (AB) will be indicated
by an arrow away from the pin, compression (AF) will be
indicated by an arrow toward the pin.
• The magnitude of AF is obtained from the equation
and AB is then found from
3. Analysis of Trusses
▪ Method of Joints:
Special Conditions
• When two collinear members are under compression, as indicated
in Fig. , it is necessary to add a third member to maintain alignment
of the two members and prevent buckling.
- y-direction (force F3) must be zero.
- x-direction (F1= F2) holds regardless of the angle
• If an external force with a component in the y-direction were applied
to the joint, then F3 would no longer be zero.
1) Sample Problem of Method of Joints
• Compute the force in each member of the loaded cantilever
truss by the method of joints.

Helpful Hints:
-The tension/compression designation refers to the member, not the joint.
-Draw the force arrow on the same side of the joint as the member which
exerts the force.
-Tension (arrow away) is distinguished from compression (arrow toward).
1) Sample Problem of Method of Joints
Helpful Hints:
-The tension/compression designation refers to the member, not the joint.
-Draw the force arrow on the same side of the joint as the member which
exerts the force.
-Tension (arrow away) is distinguished from compression (arrow toward).
1) Sample Problem of Method of Joints
Solution:
If it were not desired to calculate the external reactions at D and E, the
analysis for a cantilever truss could begin with the joint at the loaded end.
The first step, compute the external forces at D and E from the free-body
diagram of the truss as a whole. The equations of equilibrium give:

Next, draw free-body diagrams showing the forces acting on each of the
connecting pins. The correctness of the assigned directions of the forces is
verified when each joint is considered in sequence. Equilibrium requires:
1) Sample Problem of Method of Joints
Solution:
Joint B must be analyzed next, since there are more than two unknown forces
on joint C. The force BC must provide an upward component, in which case
BD must balance the force to the left. Again the forces are obtained from:

Joint C now contains only two unknowns, and these are found in the same
way as before:

Finally, from joint E there results:
and the equation

Fx

0

checks.
3. Analysis of Trusses
▪ Method of Sections:
• By the method of joints analyzing , we need only two of
the three equilibrium equations because the procedures
involve concurrent forces at each joint
• The method of sections analyzing has the basic advantage
that the force in almost any desired member may be found
directly from an analysis of a section which has cut that
member
3. Analysis of Trusses
▪ Method of Sections:
• It’s not necessary to proceed with the calculation from
joint to joint until the member in question has been
reached
• In choosing a section of the truss, in general, not more
than three members whose forces are unknown should
be cut, since there are only three available independent
equilibrium relations.
3. Analysis of Trusses
▪ Method of Sections:
Illustration of the Method
• The method of sections will now be illustrated for the truss in Fig (a).
which was used in the explanation of the method of joints.
The external reactions are first computed as with the method of
joints, by considering the truss as a whole.
3. Analysis of Trusses
▪ Method of Sections:
Illustration of the Method
• Let us determine the force in the member BE, for example.
An imaginary section, indicated by the dashed line, is passed through
the truss, cutting it into two parts, Fig. (b).
• This section has cut three members whose forces are initially
unknown.
• In order for the portion of the truss on each side of the section to
remain in equilibrium, it is necessary to apply to each cut member
the force which was exerted on it by the member cut away.
• The left-hand section is in equilibrium under the action of the applied
load L, the end reaction R, and the three forces exerted on the cut
members by the right-hand section which has been removed.
2) Sample Problem of Illustration Method
• Calculate the forces induced in members KL, CL, and CB by the
20-ton load on the cantilever truss.

Helpful Hints:
-Analysis by the method of joints would necessitate working with eight joints
in order to calculate the three forces in question.
-Thus, the method of sections offers a considerable advantage in this case.
-We could have started with moments about C or P just as well, determined
CL by a force summation in either the x- or y-direction.
2) Sample Problem of Illustration Method
Solution:
- Although the vertical components of the reactions at A and M are statically
indeterminate with the two fixed supports, all members other than AM are
statically determinate.
- We may pass a section directly through members KL, CL, and CB and analyze
the portion of the truss to the left of this section as a statically determinate
rigid body.
- The free-body diagram of the portion of the truss to the left of the section
is shown. A moment sum about L quickly verifies the assignment of CB as
compression, and a moment sum about C quickly discloses that KL is in
tension. The direction of CL is not quite so obvious until we observe that KL
and CB intersect at a point P to the right of G. A moment sum about P
eliminates reference to KL and CB and shows that CL must be compressive to
balance the moment of the 20-ton force about P. With these considerations
in mind the solution becomes straightforward, as we now see how to solve
for each of the three unknowns independently of the other two.
2) Sample Problem of Illustration Method
Solution:
- Summing moments about L requires finding the moment arm.

- Next we take moments about C, which requires a calculation of cos θ.
From the given dimensions we see θ = tan-1 (5/12) so that cos θ = 12/13.
Therefore,

Finally, we may find CL by a moment sum about P, whose distance from C
is given by ,
or
2) Sample Problem of Illustration Method
Solution:

- We also need ß, which is given by

and cos ß = 0.868. We now have

Weitere ähnliche Inhalte

Was ist angesagt?

Structural analysis (method of sections)
Structural analysis (method of sections)Structural analysis (method of sections)
Structural analysis (method of sections)
physics101
 
Trusses The Method Of Sections
Trusses  The Method Of SectionsTrusses  The Method Of Sections
Trusses The Method Of Sections
Amr Hamed
 
Determinate structures
 Determinate structures Determinate structures
Determinate structures
Tarun Gehlot
 

Was ist angesagt? (20)

Structural analysis (method of sections)
Structural analysis (method of sections)Structural analysis (method of sections)
Structural analysis (method of sections)
 
A Simplified Approach to Calculating Truss Forces
A Simplified Approach to Calculating Truss ForcesA Simplified Approach to Calculating Truss Forces
A Simplified Approach to Calculating Truss Forces
 
Truss analysis by graphical method
Truss analysis by graphical methodTruss analysis by graphical method
Truss analysis by graphical method
 
8. analysis of truss part ii, method of section, by-ghumare s m
8. analysis of truss part ii,  method of section, by-ghumare s m8. analysis of truss part ii,  method of section, by-ghumare s m
8. analysis of truss part ii, method of section, by-ghumare s m
 
Structural engineering ii
Structural engineering iiStructural engineering ii
Structural engineering ii
 
Trusses The Method Of Sections
Trusses  The Method Of SectionsTrusses  The Method Of Sections
Trusses The Method Of Sections
 
Determinate structures
 Determinate structures Determinate structures
Determinate structures
 
trusses
trussestrusses
trusses
 
05-Strength of Double Angle Bolted Tension Members (Steel Structural Design &...
05-Strength of Double Angle Bolted Tension Members (Steel Structural Design &...05-Strength of Double Angle Bolted Tension Members (Steel Structural Design &...
05-Strength of Double Angle Bolted Tension Members (Steel Structural Design &...
 
Direct integration method
Direct integration methodDirect integration method
Direct integration method
 
Lecture notes on trusses
Lecture notes on trussesLecture notes on trusses
Lecture notes on trusses
 
Shear force and bending moment diagram
Shear force and bending moment diagramShear force and bending moment diagram
Shear force and bending moment diagram
 
structure problems
structure problemsstructure problems
structure problems
 
Mm210(4b)
Mm210(4b)Mm210(4b)
Mm210(4b)
 
Chapter 5-cables and arches
Chapter 5-cables and archesChapter 5-cables and arches
Chapter 5-cables and arches
 
Moment Distribution Method
Moment Distribution MethodMoment Distribution Method
Moment Distribution Method
 
14 three moment equation
14 three moment equation14 three moment equation
14 three moment equation
 
Shear and Bending Moment in Beams
Shear and Bending Moment in BeamsShear and Bending Moment in Beams
Shear and Bending Moment in Beams
 
Macaulay's Method & Poisson's Ratio
Macaulay's Method & Poisson's  RatioMacaulay's Method & Poisson's  Ratio
Macaulay's Method & Poisson's Ratio
 
Truss-method of joints
Truss-method of joints Truss-method of joints
Truss-method of joints
 

Andere mochten auch (12)

Truss bridge final presentation
Truss bridge final presentationTruss bridge final presentation
Truss bridge final presentation
 
Roofs and truss
Roofs and trussRoofs and truss
Roofs and truss
 
Trusses
TrussesTrusses
Trusses
 
Truss analysis
Truss analysisTruss analysis
Truss analysis
 
Truss bridge final presentation
Truss bridge final presentationTruss bridge final presentation
Truss bridge final presentation
 
Centroides
CentroidesCentroides
Centroides
 
1 e bil - structures - 2nd part - types of structures
1 e bil - structures - 2nd part - types of structures1 e bil - structures - 2nd part - types of structures
1 e bil - structures - 2nd part - types of structures
 
Long span structures
Long span structures  Long span structures
Long span structures
 
truses and frame
 truses and frame truses and frame
truses and frame
 
Types roof trusses
Types roof trussesTypes roof trusses
Types roof trusses
 
Long span structures in Concrete and Steel
Long span structures in Concrete and SteelLong span structures in Concrete and Steel
Long span structures in Concrete and Steel
 
Lecture notes complex and space trusses
Lecture notes complex and space trussesLecture notes complex and space trusses
Lecture notes complex and space trusses
 

Ähnlich wie 3 analysis

Analysisi of Various Truss - Analysis 1-2.pdf
Analysisi of Various Truss - Analysis 1-2.pdfAnalysisi of Various Truss - Analysis 1-2.pdf
Analysisi of Various Truss - Analysis 1-2.pdf
ajgoal14968
 

Ähnlich wie 3 analysis (20)

Analysis of plane truss unit 5
Analysis of plane  truss unit 5Analysis of plane  truss unit 5
Analysis of plane truss unit 5
 
Trusses.pdf
Trusses.pdfTrusses.pdf
Trusses.pdf
 
Trusses
TrussesTrusses
Trusses
 
TRUSS ANALYSIS (TERM PAPER REPORT)
TRUSS ANALYSIS (TERM PAPER REPORT)TRUSS ANALYSIS (TERM PAPER REPORT)
TRUSS ANALYSIS (TERM PAPER REPORT)
 
analisa struktur indo
analisa struktur indoanalisa struktur indo
analisa struktur indo
 
Trusses
TrussesTrusses
Trusses
 
Trusses
TrussesTrusses
Trusses
 
Trusses
TrussesTrusses
Trusses
 
Trusses
TrussesTrusses
Trusses
 
Chapter 4_Engineering Structures_Review.pptx
Chapter 4_Engineering Structures_Review.pptxChapter 4_Engineering Structures_Review.pptx
Chapter 4_Engineering Structures_Review.pptx
 
L04 5.pdf (trusses)
L04 5.pdf (trusses)L04 5.pdf (trusses)
L04 5.pdf (trusses)
 
Truss
TrussTruss
Truss
 
Truss.pptx
Truss.pptxTruss.pptx
Truss.pptx
 
Analysisi of Various Truss - Analysis 1-2.pdf
Analysisi of Various Truss - Analysis 1-2.pdfAnalysisi of Various Truss - Analysis 1-2.pdf
Analysisi of Various Truss - Analysis 1-2.pdf
 
chap3_equilibrium.pdf
chap3_equilibrium.pdfchap3_equilibrium.pdf
chap3_equilibrium.pdf
 
Truss
TrussTruss
Truss
 
Engineering Mechanics Chapter 5 Equilibrium of a Rigid Body
Engineering Mechanics  Chapter 5  Equilibrium of a Rigid BodyEngineering Mechanics  Chapter 5  Equilibrium of a Rigid Body
Engineering Mechanics Chapter 5 Equilibrium of a Rigid Body
 
Desplazamientos estructura conjugada
Desplazamientos estructura conjugadaDesplazamientos estructura conjugada
Desplazamientos estructura conjugada
 
module 2 (Mechanics)
module 2 (Mechanics)module 2 (Mechanics)
module 2 (Mechanics)
 
Chapter1 ME slid show (2).pptx
Chapter1 ME slid show (2).pptxChapter1 ME slid show (2).pptx
Chapter1 ME slid show (2).pptx
 

Mehr von Mr Patrick NIYISHAKA (20)

Summary
SummarySummary
Summary
 
3 summary
3 summary3 summary
3 summary
 
2 ddb architecture
2 ddb architecture2 ddb architecture
2 ddb architecture
 
1 ddb
1 ddb1 ddb
1 ddb
 
2 countermeasures
2 countermeasures2 countermeasures
2 countermeasures
 
2 countermeasures
2 countermeasures2 countermeasures
2 countermeasures
 
3 summary
3 summary3 summary
3 summary
 
1 db security
1 db security1 db security
1 db security
 
4 summary
4 summary4 summary
4 summary
 
3 summary
3 summary3 summary
3 summary
 
2 con control
2 con control2 con control
2 con control
 
1 con exe
1 con exe1 con exe
1 con exe
 
1 basic concepts
1 basic concepts1 basic concepts
1 basic concepts
 
2 recovery
2 recovery2 recovery
2 recovery
 
3 transaction
3 transaction3 transaction
3 transaction
 
3 summary
3 summary3 summary
3 summary
 
1 query processing
1 query processing1 query processing
1 query processing
 
1 query processing
1 query processing1 query processing
1 query processing
 
2 optimization
2 optimization2 optimization
2 optimization
 
2 collision
2 collision2 collision
2 collision
 

Kürzlich hochgeladen

Kürzlich hochgeladen (20)

MINDCTI Revenue Release Quarter One 2024
MINDCTI Revenue Release Quarter One 2024MINDCTI Revenue Release Quarter One 2024
MINDCTI Revenue Release Quarter One 2024
 
Apidays Singapore 2024 - Scalable LLM APIs for AI and Generative AI Applicati...
Apidays Singapore 2024 - Scalable LLM APIs for AI and Generative AI Applicati...Apidays Singapore 2024 - Scalable LLM APIs for AI and Generative AI Applicati...
Apidays Singapore 2024 - Scalable LLM APIs for AI and Generative AI Applicati...
 
Apidays New York 2024 - Scaling API-first by Ian Reasor and Radu Cotescu, Adobe
Apidays New York 2024 - Scaling API-first by Ian Reasor and Radu Cotescu, AdobeApidays New York 2024 - Scaling API-first by Ian Reasor and Radu Cotescu, Adobe
Apidays New York 2024 - Scaling API-first by Ian Reasor and Radu Cotescu, Adobe
 
Artificial Intelligence Chap.5 : Uncertainty
Artificial Intelligence Chap.5 : UncertaintyArtificial Intelligence Chap.5 : Uncertainty
Artificial Intelligence Chap.5 : Uncertainty
 
Automating Google Workspace (GWS) & more with Apps Script
Automating Google Workspace (GWS) & more with Apps ScriptAutomating Google Workspace (GWS) & more with Apps Script
Automating Google Workspace (GWS) & more with Apps Script
 
Strategies for Unlocking Knowledge Management in Microsoft 365 in the Copilot...
Strategies for Unlocking Knowledge Management in Microsoft 365 in the Copilot...Strategies for Unlocking Knowledge Management in Microsoft 365 in the Copilot...
Strategies for Unlocking Knowledge Management in Microsoft 365 in the Copilot...
 
ProductAnonymous-April2024-WinProductDiscovery-MelissaKlemke
ProductAnonymous-April2024-WinProductDiscovery-MelissaKlemkeProductAnonymous-April2024-WinProductDiscovery-MelissaKlemke
ProductAnonymous-April2024-WinProductDiscovery-MelissaKlemke
 
Axa Assurance Maroc - Insurer Innovation Award 2024
Axa Assurance Maroc - Insurer Innovation Award 2024Axa Assurance Maroc - Insurer Innovation Award 2024
Axa Assurance Maroc - Insurer Innovation Award 2024
 
AWS Community Day CPH - Three problems of Terraform
AWS Community Day CPH - Three problems of TerraformAWS Community Day CPH - Three problems of Terraform
AWS Community Day CPH - Three problems of Terraform
 
Apidays Singapore 2024 - Modernizing Securities Finance by Madhu Subbu
Apidays Singapore 2024 - Modernizing Securities Finance by Madhu SubbuApidays Singapore 2024 - Modernizing Securities Finance by Madhu Subbu
Apidays Singapore 2024 - Modernizing Securities Finance by Madhu Subbu
 
MS Copilot expands with MS Graph connectors
MS Copilot expands with MS Graph connectorsMS Copilot expands with MS Graph connectors
MS Copilot expands with MS Graph connectors
 
Manulife - Insurer Transformation Award 2024
Manulife - Insurer Transformation Award 2024Manulife - Insurer Transformation Award 2024
Manulife - Insurer Transformation Award 2024
 
A Year of the Servo Reboot: Where Are We Now?
A Year of the Servo Reboot: Where Are We Now?A Year of the Servo Reboot: Where Are We Now?
A Year of the Servo Reboot: Where Are We Now?
 
ICT role in 21st century education and its challenges
ICT role in 21st century education and its challengesICT role in 21st century education and its challenges
ICT role in 21st century education and its challenges
 
Mastering MySQL Database Architecture: Deep Dive into MySQL Shell and MySQL R...
Mastering MySQL Database Architecture: Deep Dive into MySQL Shell and MySQL R...Mastering MySQL Database Architecture: Deep Dive into MySQL Shell and MySQL R...
Mastering MySQL Database Architecture: Deep Dive into MySQL Shell and MySQL R...
 
2024: Domino Containers - The Next Step. News from the Domino Container commu...
2024: Domino Containers - The Next Step. News from the Domino Container commu...2024: Domino Containers - The Next Step. News from the Domino Container commu...
2024: Domino Containers - The Next Step. News from the Domino Container commu...
 
Emergent Methods: Multi-lingual narrative tracking in the news - real-time ex...
Emergent Methods: Multi-lingual narrative tracking in the news - real-time ex...Emergent Methods: Multi-lingual narrative tracking in the news - real-time ex...
Emergent Methods: Multi-lingual narrative tracking in the news - real-time ex...
 
A Beginners Guide to Building a RAG App Using Open Source Milvus
A Beginners Guide to Building a RAG App Using Open Source MilvusA Beginners Guide to Building a RAG App Using Open Source Milvus
A Beginners Guide to Building a RAG App Using Open Source Milvus
 
Web Form Automation for Bonterra Impact Management (fka Social Solutions Apri...
Web Form Automation for Bonterra Impact Management (fka Social Solutions Apri...Web Form Automation for Bonterra Impact Management (fka Social Solutions Apri...
Web Form Automation for Bonterra Impact Management (fka Social Solutions Apri...
 
Exploring the Future Potential of AI-Enabled Smartphone Processors
Exploring the Future Potential of AI-Enabled Smartphone ProcessorsExploring the Future Potential of AI-Enabled Smartphone Processors
Exploring the Future Potential of AI-Enabled Smartphone Processors
 

3 analysis

  • 1. 3. Analysis of Trusses ▪ Method of Joints: • For the forces acting on the connecting pin of each joint, - First, finding the forces in the members of a truss consists of satisfying the conditions of equilibrium. - Therefore, deals with the equilibrium of concurrent forces, - And only two independent equilibrium equations are involved.
  • 2. 3. Analysis of Trusses ▪ Method of Joints: • Begin the analysis with any joint , - Where at least one known load exists and where not more than two unknown. • Usually designate the force in each member by the two letters defining the ends of the member forces are present. • The solution may be started with the pin at the left end.
  • 3. 3. Analysis of Trusses ▪ Method of Joints: • Free-body diagram is shown in Fig. • Portions of members AF and AB are shown to indicate the mechanism of the action and reaction.
  • 4. 3. Analysis of Trusses ▪ Method of Joints: • AB makes contact on the left side of the pin. If we consistently draw the force arrows on the same side of the pin as the member, then tension (AB) will be indicated by an arrow away from the pin, compression (AF) will be indicated by an arrow toward the pin. • The magnitude of AF is obtained from the equation and AB is then found from
  • 5. 3. Analysis of Trusses ▪ Method of Joints: Special Conditions • When two collinear members are under compression, as indicated in Fig. , it is necessary to add a third member to maintain alignment of the two members and prevent buckling. - y-direction (force F3) must be zero. - x-direction (F1= F2) holds regardless of the angle • If an external force with a component in the y-direction were applied to the joint, then F3 would no longer be zero.
  • 6. 1) Sample Problem of Method of Joints • Compute the force in each member of the loaded cantilever truss by the method of joints. Helpful Hints: -The tension/compression designation refers to the member, not the joint. -Draw the force arrow on the same side of the joint as the member which exerts the force. -Tension (arrow away) is distinguished from compression (arrow toward).
  • 7. 1) Sample Problem of Method of Joints Helpful Hints: -The tension/compression designation refers to the member, not the joint. -Draw the force arrow on the same side of the joint as the member which exerts the force. -Tension (arrow away) is distinguished from compression (arrow toward).
  • 8. 1) Sample Problem of Method of Joints Solution: If it were not desired to calculate the external reactions at D and E, the analysis for a cantilever truss could begin with the joint at the loaded end. The first step, compute the external forces at D and E from the free-body diagram of the truss as a whole. The equations of equilibrium give: Next, draw free-body diagrams showing the forces acting on each of the connecting pins. The correctness of the assigned directions of the forces is verified when each joint is considered in sequence. Equilibrium requires:
  • 9. 1) Sample Problem of Method of Joints Solution: Joint B must be analyzed next, since there are more than two unknown forces on joint C. The force BC must provide an upward component, in which case BD must balance the force to the left. Again the forces are obtained from: Joint C now contains only two unknowns, and these are found in the same way as before: Finally, from joint E there results: and the equation Fx 0 checks.
  • 10. 3. Analysis of Trusses ▪ Method of Sections: • By the method of joints analyzing , we need only two of the three equilibrium equations because the procedures involve concurrent forces at each joint • The method of sections analyzing has the basic advantage that the force in almost any desired member may be found directly from an analysis of a section which has cut that member
  • 11. 3. Analysis of Trusses ▪ Method of Sections: • It’s not necessary to proceed with the calculation from joint to joint until the member in question has been reached • In choosing a section of the truss, in general, not more than three members whose forces are unknown should be cut, since there are only three available independent equilibrium relations.
  • 12. 3. Analysis of Trusses ▪ Method of Sections: Illustration of the Method • The method of sections will now be illustrated for the truss in Fig (a). which was used in the explanation of the method of joints. The external reactions are first computed as with the method of joints, by considering the truss as a whole.
  • 13. 3. Analysis of Trusses ▪ Method of Sections: Illustration of the Method • Let us determine the force in the member BE, for example. An imaginary section, indicated by the dashed line, is passed through the truss, cutting it into two parts, Fig. (b). • This section has cut three members whose forces are initially unknown. • In order for the portion of the truss on each side of the section to remain in equilibrium, it is necessary to apply to each cut member the force which was exerted on it by the member cut away. • The left-hand section is in equilibrium under the action of the applied load L, the end reaction R, and the three forces exerted on the cut members by the right-hand section which has been removed.
  • 14. 2) Sample Problem of Illustration Method • Calculate the forces induced in members KL, CL, and CB by the 20-ton load on the cantilever truss. Helpful Hints: -Analysis by the method of joints would necessitate working with eight joints in order to calculate the three forces in question. -Thus, the method of sections offers a considerable advantage in this case. -We could have started with moments about C or P just as well, determined CL by a force summation in either the x- or y-direction.
  • 15. 2) Sample Problem of Illustration Method Solution: - Although the vertical components of the reactions at A and M are statically indeterminate with the two fixed supports, all members other than AM are statically determinate. - We may pass a section directly through members KL, CL, and CB and analyze the portion of the truss to the left of this section as a statically determinate rigid body. - The free-body diagram of the portion of the truss to the left of the section is shown. A moment sum about L quickly verifies the assignment of CB as compression, and a moment sum about C quickly discloses that KL is in tension. The direction of CL is not quite so obvious until we observe that KL and CB intersect at a point P to the right of G. A moment sum about P eliminates reference to KL and CB and shows that CL must be compressive to balance the moment of the 20-ton force about P. With these considerations in mind the solution becomes straightforward, as we now see how to solve for each of the three unknowns independently of the other two.
  • 16. 2) Sample Problem of Illustration Method Solution: - Summing moments about L requires finding the moment arm. - Next we take moments about C, which requires a calculation of cos θ. From the given dimensions we see θ = tan-1 (5/12) so that cos θ = 12/13. Therefore, Finally, we may find CL by a moment sum about P, whose distance from C is given by , or
  • 17. 2) Sample Problem of Illustration Method Solution: - We also need ß, which is given by and cos ß = 0.868. We now have