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rocket_fin_model
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0 Geometries 0 Meshes 0 Simulation setups 0 ResultsAbout this project
This project focuses on analyzing a rocket fin using the Finite Element Method. The fin geometry and material properties are defined, followed by applying aerodynamic loads and supports. Mesh studies are performed using different mesh sizes to compare results. Von Mises stress, deformation, and critical regions are analyzed. Finally, the factor of safety is calculated to determine structural reliability.
