Turbulent Boundary Layer Skin Friction, Heat Transfer and Pressure Measurements on Hypersonic Inlet Compression Surfaces

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Report Number: AFFDL TR 68-102
Author(s): Ryder, M. O., Jr.
Corporate Author(s): Cornell Aeronautical Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-07
Pages: 144
Contract: F33615-67-C-1203
DoD Project: 1366
Identifier: AD0672836

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Provenance: Lockheed Martin Missiles & Fire Control

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