Experimental research on the thermal throat of rocket based combined cycle combustor
Yajun Wang, Fei Qin, Zongqi Xie, Duo Zhang, Xianggeng Wei, Guoqiang He
Topics & Concepts
Mach numberCombustorMechanicsAirflowThermalSpecific impulseHypersonic speedCombustion chamberAerospace engineeringCombustionMaterials scienceMechanical engineeringEngineeringThrustMeteorologyPhysicsChemistryOrganic chemistryRocket and propulsion systems researchComputational Fluid Dynamics and AerodynamicsCombustion and flame dynamics