Aerodynamic control of supersonic inlets for optimum performance
Flow field effects on static stability and control at high supersonic Mach numbers
Factors affecting the maximum lift-drag ratio at high supersonic speeds
Reduction of wave drag of wing-body combinations at supersonic speeds through body distortions
Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
Spinning and related problems at high angles of attack for high speed airplanes