Include Page | ||||
---|---|---|---|---|
|
Include Page | ||||
---|---|---|---|---|
|
Physics Setup
Next, we will apply the boundary conditions to the geometry.
HTML |
---|
<iframe width="560" height="315" src="https://www.youtube.com/embed/_OTkN0yM4r4?rel=0" frameborder="0" allowfullscreen></iframe> |
...
Summary of steps in above video:
- Change the material of the wing to a new material with the name Aluminum 6061-T6
- Add a density property of 2700 kg/m^3
- Add an Isotropic Elasticity property, with Young's Modulus = 1e7 psi and Poisson's ratio = 0.33
- Add a fixed support on two edges of the wing's end
Go to Step 5: Numerical SolutionResults
Go to all ( ANSYS or FLUENT) AIM Learning Modules