Physics Setup

Next, we will apply the boundary conditions to the geometry.

<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 Results

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