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Advanced high temperature heat flux sensorsTo fully characterize advanced high temperature heat flux sensors, calibration and testing is required at full engine temperature. This required the development of unique high temperature heat flux test facilities. These facilities were developed, are in place, and are being used for advanced heat flux sensor development.
Document ID
19840008425
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Atkinson, W. (Pratt and Whitney Aircraft Group East Hartford, Conn., United States)
Hobart, H. F. (NASA Lewis Research Center Cleveland, OH, United States)
Strange, R. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-83526
NAS 1.15:83526
E-1891
Report Number: NASA-TM-83526
Report Number: NAS 1.15:83526
Report Number: E-1891
Meeting Information
Meeting: Intern. Conf. of the Instrument Society of America, ISA ''83
Location: Houston, TX
Country: United States
Start Date: October 10, 1983
End Date: October 13, 1983
Accession Number
84N16493
Funding Number(s)
PROJECT: RTOP 505-31-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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