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

Geometry

 

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For this problem, we are going to import the geometry into ANSYS from a CAD package. Download the part file here. Save the file somewhere convenient, like your desktop or your working directory.


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<iframe width="560" height="315" src="https://www.youtube.com/embed/z9S_UVZf0BI?rel=0-sYB6VRyp7w" frameborder="0" allowfullscreen></iframe>

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Summary of steps in above video:

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  • Open Geometry, and specify the thickness of the wing surface to be 0.01m

 

Go to Step 3: Mesh

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