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Development of heat flux sensors in turbine airfoilsThe objective is to develop heat flux sensors suitable for use on turbine airfoils and to verify the operation of the heat flux measurement techniques through laboratory experiments. The requirements for a program to investigate the measurement of heat flux on airfoils in areas of strong non-one-dimensional flow were also identified.
Document ID
19870001753
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Atkinson, W. H.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Strange, R. R.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984
Subject Category
Instrumentation And Photography
Accession Number
87N11186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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