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Dynamic gas temperature measurement system. Volume 2: Operation and program manualThe hot section technology (HOST) dynamic gas temperature measurement system computer program acquires data from two type B thermocouples of different diameters. The analysis method determines the in situ value of an aerodynamic parameter T, containing the heat transfer coefficient from the transfer function of the two thermocouples. This aerodynamic parameter is used to compute a fequency response spectrum and compensate the dynamic portion of the signal of the smaller thermocouple. The calculations for the aerodynamic parameter and the data compensation technique are discussed. Compensated data are presented in either the time or frequency domain, time domain data as dynamic temperature vs time, or frequency domain data.
Document ID
19860006181
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Purpura, P. T.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1983
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-168267-VOL-2
NAS 1.26:168267-VOL-2
Report Number: NASA-CR-168267-VOL-2
Report Number: NAS 1.26:168267-VOL-2
Accession Number
86N15651
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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