Investigation of full-scale porous injector plate transpiration cooling coupled with combustion in high-thrust H2/O2 rocket engines
Ping Jin, Zhiwei Chen, Jiguo Sun, Guobiao Cai
Topics & Concepts
Liquid-propellant rocketRocket engineInjectorCoolantRocket (weapon)MechanicsMaterials scienceMass flow rateThrustCombustion chamberHeat fluxInternal combustion engine coolingHeat transferNuclear engineeringCombustionAerospace engineeringMechanical engineeringPropellantEngineeringChemistryPhysicsOrganic chemistryRocket and propulsion systems researchHeat transfer and supercritical fluidsGas Dynamics and Kinetic Theory