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The role of freestream turbulence scale in subsonic flow separationThe ojective of this work is the clarification of the role of freestream turbulence scale in determining the location of boundary layer separation. An airfoil in subsonic wind tunnel flow is the specific case studied. Hot-film and hot-wire anemometry, liquid-film visualization and pressure measurements are the principal diagnostic techniques in use. The Vanderbilt University subsonic wind tunnel is the flow facility being used.
Document ID
19850004562
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Potter, J. L. (Vanderbilt Univ. Nashville, TN, United States)
Seebaugh, W. R. (Vanderbilt Univ. Nashville, TN, United States)
Barnett, R. J. (Vanderbilt Univ. Nashville, TN, United States)
Gokhale, R. B. (Vanderbilt Univ. Nashville, TN, United States)
Date Acquired
September 5, 2013
Publication Date
December 31, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:174172
IPR-1
NASA-CR-174172
Report Number: NAS 1.26:174172
Report Number: IPR-1
Report Number: NASA-CR-174172
Accession Number
85N12870
Funding Number(s)
CONTRACT_GRANT: NAG1-483
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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