MAE: 4700 Wing Project

Description:

This page has helpful resources for the MAE 4700/5700 Wing Design Project.

Here is the .txt file used in the video below:

NACA_0012_Airfoil.txt

The video at the link below shows you how to create the initial wing geometry in Ansys Discovery. 

The video at the link below shows you how to set up the initial wing analysis in Ansys Mechanical. 

Reiterate with varying numbers of spars/ribs, varying locations, and different thicknesses. For optimizing thickness, you can use Response Surface Optimization. This tutorial should help:

https://confluence.cornell.edu/display/SIMULATION/ANSYS+-+Plate+With+a+Hole+Optimization