Analysis of effect of tail-pipe-burner design parameters on thrust-augmentation
Experimental investigation of thrust augmentation by water-alcohol injection
West Point : A History of the United States Military Academy
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles
Spinning and related problems at high angles of attack for high speed airplanes
Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
Flow field effects on static stability and control at high supersonic Mach numbers
Factors affecting the maximum lift-drag ratio at high supersonic speeds