NASA STI Repository (National Aeronautics and Space Administration) · 1969 · 19 citations · 0 references
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Natural SciencesAerospace EngineeringPhysicsAerodynamicsFluid DynamicsBoundary Layer FlowBoundary LayersBoundary-layer StructureBoundary-layer TheoryFlow SeparationTurbulent FlowCompressible Boundary LayersHigh-reynolds-number FlowReynolds NumberReynolds Number EffectsSeparation In Turbulent Boundary LayersSupersonic Boundary LayersSupersonic FlowTurbulent Boundary Layers
Mach number effects on pressure caused incipient separation of turbulent boundary layer in two dimensional supersonic corner flow