Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects
Eagle, Walter; Driscoll, James; Benek, Jack
2011
Citation: Eagle, Walter; Driscoll, James; Benek, Jack (2011). "Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects." 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4-7, 2011, AIAA-2011-857.
Other Identifiers: AIAA-2011-857
Handle: http://hdl.handle.net/2027.42/90617
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