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PROPELLER & FAN DESIGN
USING CFD OPTIMIZATION
DAVID SHORT & ARNAUD GIRIN
DAVID SHORT
Application Engineer
2+ years experience in CFD & FEA application
engineering. Coming from a marine
engineering background, he has knowledge of
both solid mechanics and fluid dynamics.
ARNAUD GIRIN
Application Engineer
CFD & FEA engineer with extensive expertise
in a wide range of applications. More than
seven years of experience in industrial rotating
equipment design and manufacturing.
1. Benefits of Using Simulation
2. Introduction to SimScale
3. Propeller Design Using CFD
4. Live Demonstration
5. Results Summary
6. Q & A
ACCELERATE YOUR
DESIGN PROCESS
Easily test performance, optimize
durability or improve design efficiency
with cloud-based simulation.
ALL-IN-ONE
Structural mechanics,
fluid dynamics, and
thermodynamics.
REAL-TIME SUPPORT
Chat, phone and email.
Consultancy, webinars,
and training.
COLLABORATION
Join the community,
benefit from public projects,
and share know-how.
FAST & EASY
Get results faster
on any device thanks
to cloud technology.
COST-EFFICIENT
Start risk-free without
an upfront investment.
SECURE
High security with
government-approved
Advanced Encryption
Standard (AES).
PROPELLER AND FAN DESIGN: TOPIC OVERVIEW
Blades and shroudings can be optimized to
maximize the power output of a device
whilst minimizing losses due to flow
inefficiencies. CFD provides a great solution
for carrying out fast iterations in order to
converge on an optimum design without the
need for excessive physical prototyping.
When it comes to hydrodynamic
or aerodynamic design of
propellers and fans, “efficiency”
is the name of the game.
PROPELLER DESIGN EFFICIENCY
The efficiency of a propeller can be defined as:
Where:
● Thrust in N
● Axial Speed in m/s
● Resistance torque in Nm
● Rotational Speed in rev/s
PROPELLER DESIGN EFFICIENCY
How we will be calculating this efficiency:
Where:
● T: Thrust in N
● D: Propeller Diameter in m
● Q: Torque in Nm
● n: Rotational in rev/s
● ⍴: density in m3
/kg
● V: Freestream in m/s
Thrust Coefficient
Power coefficient
Advance coefficient
Torque coefficient
DESIGN PARAMETERS
● Number of blades
● Outer diameter
● Pitch- Affecting angle of attack
● Leading edge blade angle
● Trailing edge blade angle
Design parameters can impact the
performance of the propellers or fans. These
include (but aren’t limited to):
OUR CASE: PROPELLER AT MULTIPLE RPM
● Simulate the airflow passing
over the blades
● Observe the turbulences
created by the rotating motion
● Quantify the performance
indicators such as the torque,
the axial thrust, and the velocity
of the flow
● Determine loading forces acting
on the blades
Objectives
CAD IMPORT
Upload your CAD model
or import it from other cloud
services into SimScale.
SIMULATION SETUP
All steps to define and run
a simulation are done
within SimScale.
DESIGN DECISION
Use the simulation insights
to make better and faster
design decisions.
1 2 3
CAD IMPORT
Rotating region solid geometry
(this allows us to create a
rotating zone and specify an
rotational speed input)
Propeller solid
geometry
CAD Preparation
Model made of 2 solid
bodies ready to be
imported into SimScale
CAD IMPORT
Rotating Region
Using the MRF method, we can
input an angular velocity for
multiple rpm to the volume
surrounding the rotating blades
Propeller Geometry
SIMULATION SETUP
THE CAD MODEL AND MESH
Mesh Generation: Hex-dominant and Refinement
● Specific refinement applied to the blades and
the wake region. Boundary mesh layers are
adding to the propeller surfaces.
● 6.4 million cells
External Domain
A background mesh box is created to
simulate an external domain.
Analysis Type
● Incompressible analysis
● Steady state
● K-omega SST turbulence model
Boundary conditions
● Velocity Inlet
● Pressure outlet
● Slip walls walls for far field
● Non-slip walls are assigned to surfaces
of the duct and propeller
● MRF Rotating zone 6000 rpm(628
rad/s)
SIMULATION SETUP
Velocity Inlet
Pressure outlet
EXTRACT THRUST AND TORQUE
Extract thrust and torque values for each operational condition using the
“forces and moments” result control
EFFICIENCY CURVES AT DIFFERENT FREE STREAM VALUES
Efficiency values for various rpm at 4 m/s free stream velocity
EFFICIENCY CURVES AT DIFFERENT FREE STREAM VALUES
Efficiency values for various rpm at 6 m/s free stream velocity
Propeller & Fan Design Optimization via CFD

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Propeller & Fan Design Optimization via CFD

  • 1. PROPELLER & FAN DESIGN USING CFD OPTIMIZATION DAVID SHORT & ARNAUD GIRIN
  • 2. DAVID SHORT Application Engineer 2+ years experience in CFD & FEA application engineering. Coming from a marine engineering background, he has knowledge of both solid mechanics and fluid dynamics.
  • 3. ARNAUD GIRIN Application Engineer CFD & FEA engineer with extensive expertise in a wide range of applications. More than seven years of experience in industrial rotating equipment design and manufacturing.
  • 4. 1. Benefits of Using Simulation 2. Introduction to SimScale 3. Propeller Design Using CFD 4. Live Demonstration 5. Results Summary 6. Q & A
  • 5.
  • 6.
  • 7.
  • 8. ACCELERATE YOUR DESIGN PROCESS Easily test performance, optimize durability or improve design efficiency with cloud-based simulation.
  • 9. ALL-IN-ONE Structural mechanics, fluid dynamics, and thermodynamics. REAL-TIME SUPPORT Chat, phone and email. Consultancy, webinars, and training. COLLABORATION Join the community, benefit from public projects, and share know-how. FAST & EASY Get results faster on any device thanks to cloud technology. COST-EFFICIENT Start risk-free without an upfront investment. SECURE High security with government-approved Advanced Encryption Standard (AES).
  • 10.
  • 11. PROPELLER AND FAN DESIGN: TOPIC OVERVIEW Blades and shroudings can be optimized to maximize the power output of a device whilst minimizing losses due to flow inefficiencies. CFD provides a great solution for carrying out fast iterations in order to converge on an optimum design without the need for excessive physical prototyping. When it comes to hydrodynamic or aerodynamic design of propellers and fans, “efficiency” is the name of the game.
  • 12. PROPELLER DESIGN EFFICIENCY The efficiency of a propeller can be defined as: Where: ● Thrust in N ● Axial Speed in m/s ● Resistance torque in Nm ● Rotational Speed in rev/s
  • 13. PROPELLER DESIGN EFFICIENCY How we will be calculating this efficiency: Where: ● T: Thrust in N ● D: Propeller Diameter in m ● Q: Torque in Nm ● n: Rotational in rev/s ● ⍴: density in m3 /kg ● V: Freestream in m/s Thrust Coefficient Power coefficient Advance coefficient Torque coefficient
  • 14. DESIGN PARAMETERS ● Number of blades ● Outer diameter ● Pitch- Affecting angle of attack ● Leading edge blade angle ● Trailing edge blade angle Design parameters can impact the performance of the propellers or fans. These include (but aren’t limited to):
  • 15. OUR CASE: PROPELLER AT MULTIPLE RPM ● Simulate the airflow passing over the blades ● Observe the turbulences created by the rotating motion ● Quantify the performance indicators such as the torque, the axial thrust, and the velocity of the flow ● Determine loading forces acting on the blades Objectives
  • 16. CAD IMPORT Upload your CAD model or import it from other cloud services into SimScale. SIMULATION SETUP All steps to define and run a simulation are done within SimScale. DESIGN DECISION Use the simulation insights to make better and faster design decisions. 1 2 3
  • 17. CAD IMPORT Rotating region solid geometry (this allows us to create a rotating zone and specify an rotational speed input) Propeller solid geometry CAD Preparation Model made of 2 solid bodies ready to be imported into SimScale
  • 18. CAD IMPORT Rotating Region Using the MRF method, we can input an angular velocity for multiple rpm to the volume surrounding the rotating blades Propeller Geometry
  • 20. THE CAD MODEL AND MESH Mesh Generation: Hex-dominant and Refinement ● Specific refinement applied to the blades and the wake region. Boundary mesh layers are adding to the propeller surfaces. ● 6.4 million cells External Domain A background mesh box is created to simulate an external domain.
  • 21. Analysis Type ● Incompressible analysis ● Steady state ● K-omega SST turbulence model Boundary conditions ● Velocity Inlet ● Pressure outlet ● Slip walls walls for far field ● Non-slip walls are assigned to surfaces of the duct and propeller ● MRF Rotating zone 6000 rpm(628 rad/s) SIMULATION SETUP Velocity Inlet Pressure outlet
  • 22.
  • 23. EXTRACT THRUST AND TORQUE Extract thrust and torque values for each operational condition using the “forces and moments” result control
  • 24. EFFICIENCY CURVES AT DIFFERENT FREE STREAM VALUES Efficiency values for various rpm at 4 m/s free stream velocity
  • 25. EFFICIENCY CURVES AT DIFFERENT FREE STREAM VALUES Efficiency values for various rpm at 6 m/s free stream velocity