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1 Geometry
2 Meshes
2 Simulation setups
3 ResultsStructural (FEM) and aerodynamic (CFD) analysis of a trapezoidal rocket fin. Root chord 100 mm, tip chord 50 mm, semi-span 70 mm, sweep 40 mm, thickness 4 mm. Includes a mesh independence study, Von Mises stress and deformation results, factor of safety calculation, and external flow analysis with pressure and velocity fields.
by slilbaekslilbaek
LeoAristocrat created this project
3 days ago
1 Geometry 2 Meshes 2 Simulation setups 3 ResultsStructural (FEM) and aerodynamic (CFD) analysis of a trapezoidal rocket fin. Root chord 100 mm, tip chord 50 mm, semi-span 70 mm, sweep 40 mm, thickness 4 mm. Includes a mesh independence study, Von Mises stress and deformation results, factor of safety calculation, and external flow analysis with pressure and velocity fields.
