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

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

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Provenance: AFRL/VACA

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