Synonyme wurden verwendet für:
HYPERSCHALL
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keywords:(HYPERSCHALL)
Local Piston Theory with Viscous Correction and Its Application
Studies on Unsteady Shock Interactions Near a Generic Scramjet Inlet
Application of PLIF to Investigate the Hypersonic Wake of a LOFTID-Relevant Model at Mach 10
A study on heat flux predictions for re-entry flight analysis
Backpressure unstart detection for a scramjet inlet based on information fusion
A novel non-ablative thermal protection system with combined spike and opposing jet concept
Transient analysis of counterflowing jet over highly blunt cone in hypersonic flow
FLEET and PLIF Velocimetry Within A Mach 10 Hypersonic Air Flow
Active flow control by a novel combinational active thermal protection for hypersonic vehicles
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
A NEW DYNAMIC LES/RANS HYBRID METHOD
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
Characterization of Disturbance Resonance in Postshock of Blunt Body in Hypersonic Flow
BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow
AERODYNAMIC HEATING RATE EVALUATION OF MACH 5 HYPERSONIC AIRPLANES
RESEARCHES ON HEAT TRANSFER CORRELATIONS OF HYDROCARBON FUEL UNDER SUPERCRITICAL PRESSURE
HOT WALL TESTING METHODOLOGY FOR IMPULSE FACILITIES
STATIC STABILITY OF THE SCRAMSPACE I MACH 8 HYPERSONIC FLIGHT EXPERIMENT
AERODYNAMIC EFFECT BROUGHT BY A STRUT-COWL SYSTEM IN A SCRAMJET ENGINE
ZEHST: ENVIRONMENTAL CHALLENGES FOR HYPERSONIC PASSENGER TRANSPORT
NUMERICAL INVESTIGATION OF A DETONATION WAVE SYSTEM IN A SCRAMJET COMBUSTOR
CONCEPT STUDY OF AN ATMOSPHERIC REENTRY USING A WINGED UNMANNED SPACE VEHICLE
IGNITION OF HYDROGEN AND HYDROCARBON IN A SUPERSONIC FLOW BY SIMULTANEOUS OPERATION OF DBD AND PJ
OSCULATING INWARD TURNING CONE WAVERIDER/INLET (OICWI) DESIGN METHODS AND EXPERIMENTAL STUDY
Simulation of Hypersonic-Shock-Wave–Laminar-Boundary-Layer Interaction over Blunt Fin
Effect of Leading-Edge Bluntness on Shockwave–Boundary-Layer Interaction in a Scramjet Intake
Experimental Verification of a Modified Cylindrical Focused Laser Differential Interferometer
Instability Results for Cone-Cylinder-Flare and Cone-Flare Hypersonic Wind-Tunnel Configurations
Numerical simulation of hypersonic flow over highly blunted cones with spike
EFFECT OF MHD SYSTEM ARRANGEMENT ON STRUCTURE OF HIGH SPEED PLASMA FLOW AROUND CONICAL BODY
DEVELOPMENT OF F4 HOTSHOT WINDTUNNEL FOR HIGH ENTHALPY SCRAMJET TESTS
OPTIMIZATION AND EXPERIMENTAL INVESTIGATION OF 2-D HYPERSONIC CURVED SHOCK COMPRESSION INLET
ADVANCED HYPERSONIC CRYO-TANKS RESEARCH IN CHATT