Structural and aerodynamic analysis of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The project evaluates stress distribution, deformation, factor of safety, pressure distribution, velocity contours, and aerodynamic performance under simulated operating conditions.
by slilbaekslilbaek
shrinidhi_08 created this project
15 days ago
Structural and aerodynamic analysis of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The project evaluates stress distribution, deformation, factor of safety, pressure distribution, velocity contours, and aerodynamic performance under simulated operating conditions.