Potentials and problems of hydrogen fueled supersonic and hypersonic aircraft.
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Witcofski, R. D.↗
Engineering topics
Witcofski, R. D.
Publications and source records attributed to Witcofski, R. D..
Experimental stability and control results at Mach 19 of an entry vehicle designed for an intermediate lift-drag ratio
Longitudinal, lateral, and directional stability and control characteristics of lifting entry vehicle at Mach number of 19
Johnston, P. J.↗
Comparative aerodynamic study of two hypersonic cruise aircraft configurations derived from trade-off studies
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Penland, J. A.↗
Effect of thickness and sweep angle on the longitudinal aerodynamic characteristics of slab delta planforms at a Mach number of 20
Effect of thickness and sweep angle on longitudinal aerodynamic characteristics of slab delta planforms at hypersonic speed
DELTA WING↗
Maximum lift-drag ratios of delta-wing-half- cone combinations at a mach number of 20 in helium
Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift
DELTA WING↗
Wing sweep and blunting effects on delta planforms at m equals 20
Wing sweep and blunting effects on delta planforms in helium flow at Mach 20
DELTA WING↗