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Rocket Fin FEM and CFD Analysis
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Statistics
1 Geometry
6 Meshes
2 Simulation setups
4 Results
1 Geometry 6 Meshes 2 Simulation setups 4 ResultsAbout this project
The objective of this project is to analyze the structural and aerodynamic performance of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD) simulations in SimScale. The FEM analysis is performed to evaluate stress distribution, deformation, and factor of safety under aerodynamic loading conditions. The CFD analysis is carried out to study airflow behavior, pressure distribution, velocity contours, and aerodynamic effects around the rocket fin. The project also includes mesh dependency studies and the application of appropriate boundary conditions to obtain accurate simulation results.
