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Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack

Report Number: AFFDL TR 66-122
Author: Nagel, A. L.
Author: Savage, R. T.
Author: Wanner, R.
Author: Blank, R. W.
Corporate Author: The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-08
Pages: 204
Contract: AF 33(615)-2011
Project: 1366
Task: 136606
AD Number: AD0803781

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