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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
Minimum wave drag for arbitrary arrangements of wings and bodies
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