Boundary Layer Flows Over Sharp And Spherically Blunted Cones At Angle Of Attack To Supersonic Nonuniform Free Streams Volume I Analysis And Results

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Separated Flow Studies

This report reviews the progress over the last decade on separated flows conducted at these laboratories. Experimental investigations conducted in the hypersonic wind tunnels is discussed. Advancements are summarized in the theoretical area which cover the development of interacting boundary layers to the numerical computation of the complete Navier-Stokes equations.