Analysis of effect of tail-pipe-burner design parameters on thrust-augmentation
Experimental investigation of thrust augmentation by water-alcohol injection
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles
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
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