Quantitative Heat Transfer Measurement using Liquid Crystal Thermography in an Hypersonic Gun Tunnel
Prediction of Shock Angles Caused by Sharp Delta Wings with Attack Angle (TN)
FULL-LENGTH PAPERS - Viscous Compressible Flow Across a Hole in a Plate
Passive control of shock wave-boundary-layer interactions
INTERDISCIPLINARY TOPICS - Geometries for Five-Hole-Type Probes with Planar Sensor Arrays (TN)
ENGINEERING NOTES - Viscous Compressible Flow Through a Hole in a Plate, Including Entry Effects
ERRATA - Effect of Surface Roughness on Unseparated Shock-Wave-Turbulent Boundary-Layer Interactions