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Further development of the dynamic gas temperature measurement system. Volume 1: Technical effortsA compensated dynamic gas temperature thermocouple measurement method was experimentally verified. Dynamic gas temperature signals from a flow passing through a chopped-wheel signal generator and an atmospheric pressure laboratory burner were measured by the dynamic temperature sensor and other fast-response sensors. Compensated data from dynamic temperature sensor thermoelements were compared with fast-response sensors. Results from the two experiments are presented as time-dependent waveforms and spectral plots. Comparisons between compensated dynamic temperature sensor spectra and a commercially available optical fiber thermometer compensated spectra were made for the atmospheric burner experiment. Increases in precision of the measurement method require optimization of several factors, and directions for further work are identified.
Document ID
19870010253
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Elmore, D. L.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Robinson, W. W.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Watkins, W. B.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Instrumentation And Photography
Report/Patent Number
NAS 1.26:179513-VOL-1
NASA-CR-179513-VOL-1
P/W/GPD-FR-19381-VOL-1
Report Number: NAS 1.26:179513-VOL-1
Report Number: NASA-CR-179513-VOL-1
Report Number: P/W/GPD-FR-19381-VOL-1
Accession Number
87N19686
Funding Number(s)
CONTRACT_GRANT: NAS3-24228
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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