Rumman Yousaf Abbasi

Thermal computational fluid dynamics analysis of a converging-diverging rocket nozzle at varying inlet temperatures using k-w Turbulence Model

Rocket nozzles play a critical role in propulsion systems by converting thermal energy into kinetic energy to generate thrust. This study investigates the thermal and flow characteristics of a converging–diverging rocket nozzle using Computational Fluid Dynamics. The simulations were performed using the standard k-w tu...