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What is CFD Analysis of Four-Inlet Rocket Nozzle about?

This paper presents a CFD analysis of a rocket nozzle with four inlets operating at Mach 2.1, demonstrating improved performance over single and two inlet designs. The study utilizes Fluent software to analyze pressure and temperature variations in the combustion chamber, concluding that the four inlet configuration enhances efficiency. The research contributes to understanding combustion dynamics and the health evaluation of liquid-propellant rocket engines.

Author

Rohit Kaushik

Language

EN