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2 Geometries
3 Meshes
3 Simulation setups
5 ResultsThis project investigates the structural behavior of a rocket fin using the Finite Element Method (FEM). A trapezoidal rocket fin geometry was modeled and analyzed under aerodynamic loading conditions. Aluminum 6061-T6 was selected as the material due to its high strength-to-weight ratio and common aerospace applications. The study evaluates Von Mises stress, deformation, mesh convergence, and factor of safety to assess the structural integrity of the fin during flight.
by slilbaekslilbaek
vibhutipansari created this project
13 days ago
2 Geometries 3 Meshes 3 Simulation setups 5 ResultsThis project investigates the structural behavior of a rocket fin using the Finite Element Method (FEM). A trapezoidal rocket fin geometry was modeled and analyzed under aerodynamic loading conditions. Aluminum 6061-T6 was selected as the material due to its high strength-to-weight ratio and common aerospace applications. The study evaluates Von Mises stress, deformation, mesh convergence, and factor of safety to assess the structural integrity of the fin during flight.
