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  • AIM Modal Analysis of a Wing - Physics Setup

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  • 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

 



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