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0 Geometries
0 Meshes
0 Simulation setups
0 ResultsThis project involves Computational Fluid Dynamics simulation of a basic model rocket using SimScale. The objective is to analyze external airflow around the rocket, determine drag coefficient, pressure contours, and velocity distribution. The study focuses on how the rocket shape and fins affect aerodynamic performance and stability during the ascent phase.
by slilbaekslilbaek
naswiha created this project
9 days ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsThis project involves Computational Fluid Dynamics simulation of a basic model rocket using SimScale. The objective is to analyze external airflow around the rocket, determine drag coefficient, pressure contours, and velocity distribution. The study focuses on how the rocket shape and fins affect aerodynamic performance and stability during the ascent phase.
