Flow characteristics and stability of induced shock waves in the isolator of rotating detonation ramjet under flight Mach number 2.5 conditions
Qianmin Wu, Zhiyong Lin, Xixuan Huang, Dingrui Zhang
Topics & Concepts
IsolatorDetonationRamjetMach numberShock waveMechanicsOverall pressure ratioShock (circulatory)CombustorSupersonic speedScramjetOblique shockMaterials sciencePhysicsAerospace engineeringEngineeringCombustionChemistryExplosive materialElectrical engineeringInternal medicineGas compressorMedicineOrganic chemistryCombustion and Detonation ProcessesEnergetic Materials and CombustionRocket and propulsion systems research