This project aims to analyze the structural strength and aerodynamic performance of a rocket fin using the Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The study evaluates stress, deformation, pressure distribution, airflow behavior, and overall stability of the rocket fin under aerodynamic loading. The results help assess the fin's performance, safety, and design efficiency for aerospace applications.
by slilbaekslilbaek
mmine created this project
8 days ago
This project aims to analyze the structural strength and aerodynamic performance of a rocket fin using the Finite Element Method (FEM) and Computational Fluid Dynamics (CFD). The study evaluates stress, deformation, pressure distribution, airflow behavior, and overall stability of the rocket fin under aerodynamic loading. The results help assess the fin's performance, safety, and design efficiency for aerospace applications.