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Skin Friction, Heat Transfer, and Pressure Measurements on Hypersonic Inlet Compression Surfaces in the Mach Number Range 7.5 to 16Author(s): Ryder, M. O., Jr.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-12
Report number: AFFDL TR 65-199