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Measuring Laminar-Separation Bubbles On AirfoilsNonintrusive multielement heat-transfer sensor overcomes limitations of previous methods. New technique determines simultaneously extent of laminar boundary layer and locations of laminar separation, transition in separated layer, and turbulent reattachment. In tests, only small amounts of heat introduced, and heated thin films caused little disturbance to shear layer or to each other. Promising tool for measurements of stability of laminar boundary layers, separated shear layers, and transitional separation bubbles. Simple and capable of providing comprehensive picture of state of shear flow along entire surface. Significant savings in tunnel (or flight) test time with corresponding savings in cost.
Document ID
19890000371
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stack, John P.
(NASA Langley Research Center, Hampton, VA.)
Mangalam, Sivaramakrishnan M.
(Analytical Services and Materials, Inc.)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13952
Accession Number
89B10371
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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