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Comparisons of boundary-layer transition measurement techniques in the Langley Unitary Plan wind tunnelFour different boundary-layer transition detection techniques, namely liquid crystals, very thin hot films, IR photography, and an optical interferometer, were compared using the same flat plate model for the same tunnel conditions. The comparisons, conducted at NASA-Langley, involved not only their sensitivity to transition but also their ease of use. The thin films, as expected, gave excellent quantitative information and were used as the standard for evaluating the other techniques. Both the liquid crystals and IR photography were able to detect transition before the boundary-layer intermittency factor had reached 50 percent. The optical interferometer was unsuccessful. Conditions sampled included a range of Mach numbers from 1.5 to 2.5 and unit Reynolds numbers from 1.0 to 4.0 million/foot.
Document ID
19890060293
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hall, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Carraway, D. L.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, C. B.
(NASA Langley Research Center Hampton, VA, United States)
Wright, R. E., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Obara, C. J.
(Planning Research Corp. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 89-2205
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Seattle, WA
Country: United States
Start Date: July 31, 1989
End Date: August 2, 1989
Sponsors: AIAA
Accession Number
89A47664
Distribution Limits
Public
Copyright
Other

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