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1 Geometry
4 Meshes
2 Simulation setups
3 ResultsStatic structural analysis of a rocket fin using the Finite Element Method (FEM). The objective is to evaluate Von Mises stress, total deformation, mesh convergence, and factor of safety under aerodynamic loading.
by mwavinyamwavinya
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
sahaahana0462 created this project
10 days ago
1 Geometry 4 Meshes 2 Simulation setups 3 ResultsStatic structural analysis of a rocket fin using the Finite Element Method (FEM). The objective is to evaluate Von Mises stress, total deformation, mesh convergence, and factor of safety under aerodynamic loading.
