The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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

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

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Lockheed Martin Missiles & Fire Control
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