This project focuses on the design and aerodynamic analysis of a rocket fin geometry using Computational Fluid Dynamics (CFD) simulation in SimScale. The fin model is created with specific geometric parameters such as root chord, tip chord, span, sweep angle, and thickness. The designed fin is analyzed under airflow conditions to study important aerodynamic characteristics such as pressure distribution, velocity variation, and flow behavior around the fin surface. The objective of this project is to understand how fin geometry influences aerodynamic performance and stability of a rocket. The simulation results help evaluate the effectiveness of the fin design and provide insights for improving aerodynamic efficiency.
GOPIGARAVI created this project
about 2 months ago
This project focuses on the design and aerodynamic analysis of a rocket fin geometry using Computational Fluid Dynamics (CFD) simulation in SimScale. The fin model is created with specific geometric parameters such as root chord, tip chord, span, sweep angle, and thickness. The designed fin is analyzed under airflow conditions to study important aerodynamic characteristics such as pressure distribution, velocity variation, and flow behavior around the fin surface. The objective of this project is to understand how fin geometry influences aerodynamic performance and stability of a rocket. The simulation results help evaluate the effectiveness of the fin design and provide insights for improving aerodynamic efficiency.
by slilbaekslilbaek