Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack
Item
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Title
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Investigation of Boundary Layer Transition in Hypersonic Flow at Angle of Attack
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Date
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1966
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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AFFDL TR 66-122
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Creator
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Nagel, A. L.
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Savage, R. T.
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Wanner, R.
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Blank, R. W.
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Corporate Author
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The Boeing Company
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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204
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Identifier
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AD0803781
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Access Rights
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Export Controls
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Distribution Classification
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1
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Contract
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AF 33(615)-2011
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DoD Project
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1366
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DoD Task
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136606
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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AFFDL LTR
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Report Availability
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Full text available
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Date Issued
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1966-08
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Abstract
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The abstract for this report is either unavailable or has yet to be entered
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Provenance
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AFRL/VACA
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Type
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report
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Format
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1 online resource