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Hot film wall shear instrumentation for compressible boundary layer transition researchExperimental and analytical studies of hot film wall shear instrumentation were performed. A new hot film anemometer was developed and tested. The anemometer performance was not quite as good as that of commercial anemometers, but the cost was much less and testing flexibility was improved. The main focus of the project was a parametric study of the effect of sensor size and substrate material on the performance of hot film surface sensors. Both electronic and shock-induced flow experiments were performed to determine the sensitivity and frequency response of the sensors. The results are presented in Michael Moen's M.S. thesis, which is appended. A condensed form of the results was also submitted for publication.
Document ID
19930008666
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schneider, Steven P.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-191360
NAS 1.26:191360
Report Number: NASA-CR-191360
Report Number: NAS 1.26:191360
Accession Number
93N17855
Funding Number(s)
CONTRACT_GRANT: NAG1-1201
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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