Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane
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
Experimental techniques for predicting store motions during release or ejection
A review of recent information on boundary layer transition at supersonic 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