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Experimental investigation of thrust augmentation by water-alcohol injection
Analysis of effect of tail-pipe-burner design parameters on thrust-augmentation
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
Interference effects upon fuselage drag of a jet exhausting from a wing-mounted nacelle