This project analyzes the structural and aerodynamic performance of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD) in SimScale. The study evaluates Von Mises stress, deformation, factor of safety, pressure distribution, velocity contours, and airflow around the fin under aerodynamic loading. The objective is to assess the fin's structural integrity and aerodynamic behavior and investigate potential design improvements to reduce stress and drag
by slilbaekslilbaek
Trishna09 created this project
19 days ago
This project analyzes the structural and aerodynamic performance of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD) in SimScale. The study evaluates Von Mises stress, deformation, factor of safety, pressure distribution, velocity contours, and airflow around the fin under aerodynamic loading. The objective is to assess the fin's structural integrity and aerodynamic behavior and investigate potential design improvements to reduce stress and drag