Create a Pareto Optimization Study. Use design parameters from the reference
simulation as inputs for the optimization study. To define objectives for the optimization
and to compare the designs, use scenes, plots, and reports as outputs.
To launch Design Manager from the reference
simulation:
-
Right-click the root node of the simulation tree and select Create
Design Manager Project.
Simcenter STAR-CCM+
creates a new Design Manager project and imports the design parameters, reports,
scenes, plots, and monitors from the reference simulation.
-
Save the Design Manager project as
airfoilOptimizationStudy.dmprj.
To create a Pareto optimization study:
-
Right-click the Design Studies node and select
New.
-
Rename the node to Cl_vs_Cd.
-
In the Properties window, set Study
Type to Optimization.
-
Define the optimization settings for the study:
-
Select the Optimization Settings node and set
Optimization Type to Multiple Objective
Tradeoff (Pareto).
-
Set Designs to Run to 120.
-
Select the node and make sure Number of Designs is set
to 12.
The archive size determines the number of non-dominated
designs you want to find during the study to resolve the Pareto front.
The recommended
Designs to Run is 8 to 12 times the
Archive Size.
注 | When specifiying an
archive size, make sure the value is evenly divisible by four and
greater than or equal to 12. Additionally, the value should be
greater than or equal to the number of input parameters in the
study. |
-
Set the input parameters for the study to the design parameters that define the
position of the flaps:
-
Select the node.
-
In the Properties window, click
(Custom Editor) for
Parameters.
-
In the Input Parameters dialog, select
the following parameters:
Node |
Parameter |
3D-CAD Model 1 |
LeadingFlapRotateAngle
TrailingFlapRotateAngle
|
|
TranslateLeadingFlap_X TranslateLeadingFlap_Y |
|
TranslateTrailingFlap_X
TranslateTrailingFlap_Y
|
Simulation
Parameters |
ConvergenceCriterion |
注 | To avoid each
simulation running to the maximum number of steps,
ConvergeneCriterion defines a stopping
criterion based on the convergence of the lift and drag
coefficients. |
-
Click OK.
-
Define an appropriate value range for each input parameter:
-
Right-click the node and select Edit....
-
Set the following parameter properties:
Name |
Parameter Type |
Baseline Value |
Range |
Increment |
ConvergenceCriterion |
Constant |
5.0E-4 |
|
|
LeadingFlapRotateAngle |
Continuous |
5.0 deg |
[1.0, 9.0] deg |
0.1 deg |
TrailingFlapRotateAngle |
Continuous |
40.0 deg |
[36.0, 44.0] deg |
0.1 deg |
TranslateLeadingFlap_X |
Continuous |
-0.035 m |
[-0.04, -0.03] m |
5.1E-4 m |
TranslateLeadingFlap_Y |
Continuous |
0.0 m |
[-0.005, 0.005] m |
5.0E-4 m |
TranslateTrailingFlap_X |
Continuous |
-0.02 m |
[-0.025, -0.015] m |
5.1E-4 m |
TranslateTrailingFlap_Y |
Continuous |
0.05 m |
[0.045, 0.055] m |
5.1E-4 m |
-
Click Close.