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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
Effect of airplane configuration on static stability at subsonic and transonic speeds
Factors affecting the flow distortions produced by supersonic inlets
Interference effects upon fuselage drag of a jet exhausting from a wing-mounted nacelle
Flow field effects on static stability and control at high supersonic Mach numbers