Advances in hypersonic extrapolation capability - Wind tunnel to flight
Hypersonic cruise aircraft configuration reliable Reynolds numbers extrapolation from laminar boundary to turbulent layer
Penland, J. A.↗
Engineering topics
Romeo, D. J.
Publications and source records attributed to Romeo, D. J..
Experimental investigation of secondary jets from two-dimensional nozzles with various exit Mach numbers for hypersonic control application
Secondary jets from two-dimensional nozzles with various exit Mach numbers for hypersonic control application
TWO-DIMENSIONAL JET↗
Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0
Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed
AERODYNAMIC CHARACTERISTICS↗