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0 ResultsCFD analysis of a rocket nozzle to investigate the effect of throat curvature (R = 5, 10, and 15 mm) on flow characteristics, including pressure, velocity, and Mach number.
by slilbaekslilbaek
nasajylee created this project
15 days ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsCFD analysis of a rocket nozzle to investigate the effect of throat curvature (R = 5, 10, and 15 mm) on flow characteristics, including pressure, velocity, and Mach number.
