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This project focuses on the structural and aerodynamic analysis of a rocket fin using Finite Element Method (FEM) and Computational Fluid Dynamics (CFD) in SimScale. The objective is to evaluate stress distribution, deformation, factor of safety, airflow behavior, pressure distribution, and aerodynamic performance under realistic operating conditions. Mesh studies and engineering interpretations are included to assess the structural integrity and aerodynamic efficiency of the design.
by slilbaekslilbaek
Gothainayaki created this project
about 10 hours ago