6-3 Improvements of Accelerometer Force Measurement Technique
Free-flight Tests of Reentry Capsule Models in Free-piston Shock Tunnel
Free-Flight Aerodynamic Test with Projectile-Onboard Data Recorder in a Ballistic Range
Effect of Wall Catalycity on Aerodynamic Heating of Flat Plates in a High Enthalpy Shock Tunnel
STUDY ON AERODYNAMIC CHARACTERISTICS OF A HIGH ENTHALPY FLOW AROUND BLUNT-NOSED BODY
Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
AEROHEATING MEASUREMENT OF A RE-ENTRY CAPSULE MODEL IN FREE-PISTON SHOCK TUNNEL HIEST
Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight