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Incipient separation pressure rise for a Mach 3.8 turbulent boundary layer.Additional incipient separation data presented cover a range of Reynolds numbers not covered in previous investigations conducted by Seebaugh (1968) and Rose (1972). A novel technique for detecting incipient separation is discussed. Several methods for detecting separation are considered. One method is based on the introduction of alcohol at a minute rate into the boundary layer.
Document ID
19730044025
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rose, W. C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Page, R. J.
Childs, M. E.
(Washington, University Seattle, Wash., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1973
Publication Information
Publication: AIAA Journal
Volume: 11
Subject Category
Fluid Mechanics
Accession Number
73A28827
Funding Number(s)
CONTRACT_GRANT: NGR-48-002-047
Distribution Limits
Public
Copyright
Other

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