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What is Wall Heat Flux in Rocket Combustion Chamber about?

This document presents a study on wall heat fluxes in a rocket combustion chamber featuring a porous injector head, utilizing both experimental and numerical methods. The research demonstrates that the porous injector improves combustion efficiency and reduces pressure drop compared to conventional injectors, with simulations conducted using ANSYS CFX to model turbulence and combustion. Results indicate a strong correlation between experimental and numerical data, highlighting the effectiveness of the porou

Author

asdhdahgad

Language

EN