Changsha Hunan, 410073
China
National University of Defense Technology
Hypersonic flow, High-temperature real gas effects, thermochemical nonequilibrium, Shock wave/boundary layer interaction, Shock/shock interaction
regenerative cooling, sCO2, Heat Transfer Enhancement, channel material, Entropy
regenerative cooling, supercritical CO2, cross-section shape, flow pattern, channel material
Thermo-chemical nonequilibrium, High Mach number, Supersonic combustion, Two-temperature model, LES