DEVELOPING AN EMOTIONAL INTELLIGENT CONTROLLER FOR SPACE LAUNCH VEHICLE APPLICATION
DESIGN OF AN AIRFRAME INTEGRATED 3D SCRAMJET AND EXPERIMENTAL RESULTS AT A MACH 10 FLIGHT CONDITION
DESIGN OF A MINIMUM TRIM HYPERSONIC AIRBREATHING ACCELERATOR VEHICLE
DESIGN OF A CIRCULAR TO RECTANGULAR TRANSITION SCRAMJET NOZZLE WITH STREAMLINE TRACING TECHNIQUE
CONTROL-ORIENTED 3D MODELING OF FLEXIBLE HYPERSONIC VEHICLES
CONCEPT STUDY OF AN ATMOSPHERIC REENTRY USING A WINGED UNMANNED SPACE VEHICLE
CHEMILUMINESCENCE IMAGING IN A SUPERSONIC COMBUSTOR OPERATING IN RADICAL FARMING MODE
CHECKOUT TESTING OF THE NEW BASIC PROCESS CONTROL SYSTEM AT THE AERODYNAMIC AND PROPULSION TEST UNIT
CFD ANALYSIS OF UNSTEADY COMBUSTION PHENOMENA IN THE HYSHOT-II SCRAMJET CONFIGURATION
CALIBRATION OF THERMAL PAINTS FOR SURFACE TEMPERATURE MEASUREMENT OF HIFIRE-0 FLIGHT
BOUNDARY LAYER TRANSITION ON THE LEA HYPERSONIC VEHICLE FOREBODY
BLUNTNESS EFFECTS ON LIFT-TO-DRAG RATIO OF LEADING EDGES FOR HYPERSONIC WAVERIDER CONFIGURATIONS
A THERMAL ANALYSIS METHOD FOR FUEL-COOLED COMBUSTOR STRUCTURE BASED ON HEAT FLUX MEASUREMENT
ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION
APPLICATION OF THE gamma -R e~0~tTRANSITION MODEL IN HIGH SPEED FLOWS