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机译:
Harbin Inst Technol;
Low flight dynamic pressure; Fuel mixing characteristics; Flame propagation characteristics; Combustion characteristics; LIQUID-KEROSENE; NUMERICAL INVESTIGATIONS; THERMAL MANAGEMENT; STRUT; FUEL; INJECTION; MODEL; SIMULATIONS; PERFORMANCE; OXIDATION;
机译:Ignition enhancement of liquid kerosene by a novel high-energy spark igniter in scramjet combustor at Mach 4 flight condition
机译:Numerical study on the mixing and combustion characteristics of a liquid kerosene jet in a scramjet combustor
机译:Numerical investigation on the performance and combustion characteristics of a cavity based scramjet combustor with novel strut injectors
机译:Characteristics of two phase flow by dynamic image analysis in a plate heat exchanger
机译:Integration of ion-exchange chromatography fractionation with reversed-phase liquid chromatography-atmospheric pressure chemical ionization mass spectrometer and matrix-assisted laser desorption/ionization time-of-flight mass spectrometry for isolation and identification of compounds in psoralea corylifolia
机译:俄罗斯Ram / scramjets和Turboramjets的研究与开发(LaRecherche et le Developpement des statoreacteurs,des statoreacteurs a Combustion supersonique et des Turbostatoreacteurs en Russie)