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SIMULATION MOOC

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AIM Modal Analysis of a Wing - Numerical Results

Created by Madison Hill, last modified on Aug 15, 2016

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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 6: Verification and Validation

Go to all ANSYS AIM Learning Modules

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