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4
0
1 Geometry
2 Meshes
1 Simulation setup
0 ResultsThis project investigates the structural integrity and aerodynamic performance of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The fin geometry is modeled as a trapezoidal aluminum fin attached to a rocket body. Structural analysis is performed under aerodynamic pressure loading to evaluate stress distribution and deformation. CFD analysis is conducted to study airflow characteristics, pressure distribution, and velocity contours around the fin. The results help assess the fin's strength, stability, and aerodynamic efficiency during flight conditions.
Pritam0211 created this project
about 1 month ago
1 Geometry 2 Meshes 1 Simulation setup 0 ResultsThis project investigates the structural integrity and aerodynamic performance of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The fin geometry is modeled as a trapezoidal aluminum fin attached to a rocket body. Structural analysis is performed under aerodynamic pressure loading to evaluate stress distribution and deformation. CFD analysis is conducted to study airflow characteristics, pressure distribution, and velocity contours around the fin. The results help assess the fin's strength, stability, and aerodynamic efficiency during flight conditions.
