Create an aerodynamic divergence subcase

1. In the Simulation Navigator, right-click the static aeroelastic response solution node and choose New Subcase.The Solution Step dialog box opens.

2. In the Solution Step dialog box, from the Step list, select Subcase - Aeroelastic Divergence.

3. Click Create Step.The Properties, Aerodynamic Symmetry, and Boundary Condition Control Variables groups appear.

4. Click OK.

How do I

Assign a modeling object to a solution or solution subcase

Define an aerodynamic control surface

Create a static aeroelastic subcase

Define aerodynamic divergence data

Create a fictitious support

Plot trim conditions

Learn more

Static aeroelastic response analysis (SOL 144)

Aeroelastic divergence analysis workflow (SOL 144)

Aeroelastic trim analysis workflow (SOL 144)

Defining trim variables

Constraints in trim analysis

Post-processing aeroelastic trim analysis results

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Create an aerodynamic divergence subcase, Simcenter 3D 2021.1 Series

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