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Computational Fluid Dynamic (CFD) simulation of a rocket body equipped with three swept-back parallelogram stabilizing fins. This study aims to analyze airflow patterns, identify the center of pressure, and evaluate aerodynamic drag to optimize the flight stability of the rocket design.
by slilbaekslilbaek
Va_1R51071 created this project
20 days ago
Computational Fluid Dynamic (CFD) simulation of a rocket body equipped with three swept-back parallelogram stabilizing fins. This study aims to analyze airflow patterns, identify the center of pressure, and evaluate aerodynamic drag to optimize the flight stability of the rocket design.