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Experimental study of two separating turbulent boundary layersA detailed study of two strong adverse pressure gradient flows, one with a free-stream velocity of 35 m/sec, at throat (producing a Re sub theta of 27000 at detachment) and another with free-stream velocity of 22 m/sec, at throat (producing a Re sub theta of 19000 at detachment) is presented. In these examples flows separate slowly and reattach very rapidly over a very short distance in a streamwise direction. In the backflow region, there appears to be a semi-logarithmically flat region in the streamwise fluctuating velocity component, u', which spreads over a definite range of y/delta. In power spectra, the flow variables phi sub upsilon upsilon (kappa sub 1 delta)/ -uv bar sub max vs. kappa sub 1 delta forms a unique set of scaling parameters for adverse pressure gradient flows. Experimental results show good agreement with previous studies.
Document ID
19870016852
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nagabushana, K. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Simpson, R. L.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Agarwal, N. K.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:181011
NASA-CR-181011
Report Number: NAS 1.26:181011
Report Number: NASA-CR-181011
Accession Number
87N26285
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-0134-84
CONTRACT_GRANT: NAG1-446
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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