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  • AIM Modal Analysis of a Wing - Numerical Results

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Author: Madison Hill, ANSYS

Problem Specification
1. Pre-Analysis & Start-Up
2. Geometry
3. Mesh
4. Physics Setup
5. Numerical Results
6. Verification & Validation

Numerical Results

 


Summary of steps in above video:

  • Create Displacement Magnitude contours for each mode
  • Look at the calculated modal frequencies under Physics > Output > Eigenvalues
  • Refine the mesh and investigate any change in modal frequencies

 


Go to Step 7: Verification & Validation

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