AIAA Journal · 1968 · 102 citations · 5 references
Natural SciencesAerospace EngineeringFluid DynamicsPressure DistributionShock ResponseShock WavesExperimental StudiesPressure RecoveryShock Boundary-layer InteractionShock Layer StructureShock-induced SeparationStatic PressureStatic Pressure Recovery
Lip shock from separation edge of half angle wedge and resultant static pressure recovery distribution along wake
5
Near wake of a blunt body at hypersonic speeds
C. Forbes Dewey · AIAA Journal · 1965 · 75 citations
On the separation of a supersonic flow at a sharp corner.
I. S. Donaldson · AIAA Journal · 1967 · 44 citations