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AIM Modal Analysis of a Wing - Panel
AIM Modal Analysis of a Wing - Panel

Numerical Results

Here we will examine the results of our simulation.

 

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<iframe width="560" height="315" src="https://www.youtube.com/embed/5EAln4tADgk?rel=0" frameborder="0" allowfullscreen></iframe>

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  • 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 76: Verification and Validation

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