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Exercise 2: Structural FEA of Aircraft
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1 Geometry
1 Mesh
2 Simulation setups
2 Results
1 Geometry 1 Mesh 2 Simulation setups 2 ResultsAbout this project
The goal of the project is : 1. Structural FEA of Aircradt wing 2. Understanding the 2 load cases (Pressure and torsion) that causes Nonlinear deformation in the wing
