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Thermal sensing of cryogenic wind tunnel model surfaces Evaluation of silicon diodesDifferent sensors and installation techniques for surface temperature measurement of cryogenic wind tunnel models were investigated. Silicon diodes were selected for further consideration because of their good inherent accuracy. Their average absolute temperature deviation in comparison tests with standard platinum resistance thermometers was found to be 0.2 K in the range from 125 to 273 K. Subsurface temperature measurement was selected as the installation technique in order to minimize aerodynamic interference. Temperature distortion caused by an embedded silicon diode was studied numerically.
Document ID
19860052331
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Daryabeigi, K.
(Old Dominion Univ. Norfolk, VA, United States)
Ash, R. L.
(Old Dominion University Norfolk, VA, United States)
Dillon-Townes, L. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Subject Category
Instrumentation And Photography
Accession Number
86A37069
Funding Number(s)
CONTRACT_GRANT: NAS1-17099
CONTRACT_GRANT: NASA TASK 25
Distribution Limits
Public
Copyright
Other

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