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Open access Oct 2026

Numerical Analysis of Bell Rocket Nozzle Performance at Variable Ambient Pressure Conditions

This study investigates the aerodynamic performance and combustion plume structure of a baseline Rao bell rocket nozzle across launch ascent at ambient pressure conditions by Computational Fluid Dynamics (CFD) and Rocket Propulsion Analysis (RPA) methods. The baseline configuration was first analysed to investigate the...

Cormac E. Johnson, Jun Yao · 0 citations

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