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Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer modelsThe apparatus and technique for measuring the thermophysical properties of models used with the phase-change paint method for obtaining wind tunnel heat transfer data are described. The method allows rapid measurement of the combined properties in a transient manner similar to an actual wind tunnel test. An effective value of the thermophysical properties can be determined which accounts for changes in thermal properties with temperature or with depth into the model surface. The apparatus was successfully tested at various heating rates between 19,000 and 124,000 watts per square meter.
Document ID
19750002032
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Romanowski, R. F.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Steinberg, I. H.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Publication Information
Publisher: NASA
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-2434
Report Number: NASA-CR-2434
Accession Number
75N10104
Funding Number(s)
CONTRACT_GRANT: NAS1-11537
PROJECT: RTOP 760-66-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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