Experimental investigation of thrust augmentation by water-alcohol injection
Analysis of effect of tail-pipe-burner design parameters on thrust-augmentation
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles
Factors affecting the flow distortions produced by supersonic inlets
Interference effects upon fuselage drag of a jet exhausting from a wing-mounted nacelle
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
Reduction of wave drag of wing-body combinations at supersonic speeds through body distortions