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0 ResultsFEM and CFD simulation of a trapezoidal aluminium rocket fin. Structural analysis to determine Von Mises stress distribution, deformation, and factor of safety under aerodynamic loading. CFD analysis to study pressure distribution, velocity contours, and drag coefficient at 100 m/s flow. Material: Aluminium 6061-T6. Part of India SpaceLab Aerospace Simulation Workshop.
by slilbaekslilbaek
vinishaT created this project
19 days ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsFEM and CFD simulation of a trapezoidal aluminium rocket fin. Structural analysis to determine Von Mises stress distribution, deformation, and factor of safety under aerodynamic loading. CFD analysis to study pressure distribution, velocity contours, and drag coefficient at 100 m/s flow. Material: Aluminium 6061-T6. Part of India SpaceLab Aerospace Simulation Workshop.
