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Vortex boundary-layer interactionsThe interaction of a turbulent boundary layer on a flat plate with a strong artificially generated longitudinal vortex which may or may not actually enter the boundary layer is studied. The vortices are generated by a delta wing suspended ahead of the test plate, so that the configuration is approximately that of a close coupled carnard with zero main-wing sweep and an invisible body. All necessary configuration and parametric checks are completed, and data acquisition and analysis on the first configuration chosen for detailed study, in which the vortex starts to merge with the boundary layer a short distance downstream of the leading edge of the test plate, are nearly complete.
Document ID
19850027060
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bradshaw, P.
(Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
September 5, 2013
Publication Date
August 31, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-176192
NAS 1.26:176192
Report Number: NASA-CR-176192
Report Number: NAS 1.26:176192
Accession Number
85N35373
Funding Number(s)
CONTRACT_GRANT: NAGW-581
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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