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Description:

This page has helpful resources for the Fall MAE 4700 Wing Project which includes a demo video with no sound, a project outline of steps in ANSYS, and an FAQ that will be updated as questions come in.

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Please note that this video is a demonstration of me creating a simple geometry. There is no sound in the video. Creating the geometry/solution can be achieved in many different methods. This video is simply an example. 


Here is the .txt file that was used in this tutorial:

View file
nameNACA_0012_Airfoil_4Meters.txt
height250
 


Mesh: The video below has a mesh size that is much smaller than you need. Realistically, an element size of around 1 meter is a good start and will give you a reasonable mesh to explore mesh convergence with. 

Geometry Creation Video

HTML
<iframe width="560" height="315" src="https://www.youtube.com/embed/hN0-WQaMztY" frameborder="0" allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture" allowfullscreen></iframe>

Demonstration Video

HTML
<iframe width="560" height="315" src="https://www.youtube.com/embed/3UMF_X4qfs8" frameborder="0" allow="accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture" allowfullscreen></iframe>

 

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Summary of Steps:

  1. Static Structural

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    1. Add Total Deformation
    2. Add Equivalent (von-Misses)

7. Reiteration

 


Reiterate with varying numbers of spars/ribs, varying locations, and different thicknesses. For varying thickness, look at setting up a parameter. This tutorial should help:

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