A NEW METHOD FOR CALIBRATING FLOW FIELD OF HYPERSONIC NOZZLE
SIMULATION OF HIGH MACH NUMBER SCRAMJET FLOW CONDITIONS USING THE X2 EXPANSION TUBE
ANALYSIS AND CORRELATION OF FLAME STABILITY LIMITS IN SUPERSONIC FLOW WITH CAVITY FLAMEHOLDER
WATER INJECTION PRE-COMPRESSOR COOLING ASSIST SPACE ACCESS
THE THEORETICAL STUDY OF THE AERO-THERMODYNAMICS CHARACTERISTICS FOR SCRAMJET COMBUSTOR
RAPID THREE-DIMENSIONAL CONSTRAINED TRAJECTORY GENERATION FOR NEAR SPACE HYPERSONIC VEHICLES
THERMAL PROTECTION AND HYDROGEN PRODUCTION ON BOARD OF THE HYPERSONIC VEHICLE
LARGE-EDDY SIMULATION OF PSEUDO-SHOCK WAVE IN A SQUARE DUCT
ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION
MULTI-OBJECTIVE OPTIMIZATION OF HYPERSONIC VEHICLES UNDER ASYMMETRIC BOUNDARY-LAYER CONDITIONS
VALIDATION OF PIV MEASUREMENTS USING SUPERSONIC TURBULENT BOUNDARY LAYER
TOWARDS ROBUST AERO-THERMODYNAMIC PREDICTIONS FOR RE-USABLE SINGLE-STAGE TO ORBIT VEHICLES
APPLICATION OF THE gamma -R e~0~tTRANSITION MODEL IN HIGH SPEED FLOWS
EXPERIMENTAL INVESTIGATION ON COUPLING CHARACTERISTICS OF CAVITY FLAMEHOLDER AND STRUT JET
CONTROL-ORIENTED 3D MODELING OF FLEXIBLE HYPERSONIC VEHICLES
SHOCK TUBE TESTING OF THE TRANSPIRATION-COOLED HEAT SHIELD EXPERIMENT AKTIV
TURBULENT FLOW SIMULATIONS OF A MIXTURE OF PERFECT GASES