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Feasibility of generating an artificial burst in a turbulent boundary layerArtificial bursts were generated in laminar and turbulent boundary layers. The burst-like events were produced by withdrawing near-wall fluid from two minute holes separated in the spanwise direction or by pitching a miniature delta wing that was flush-mounted to the wall. Either of these actions generated streamwise vorticity and a low-speed streak that resembled a naturally occurring one. The resulting sequence of events occurred at a given location and at controlled times, allowing detailed examination and comparison with natural, random bursts by means of flow visualization and fast-response probe measurement techniques.
Document ID
19860018905
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gad-El-hak, M.
(Flow Research, Inc. Kent, WA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:4003
REPT-332
NASA-CR-4003
Accession Number
86N28377
Funding Number(s)
PROJECT: RTOP 505-60-31-04
CONTRACT_GRANT: NAS1-17951
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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