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Analysis of transient heat flow to thick-walled plates and cylindersA methodology is described for the analysis of a transient temperature measurement made in a flat or curved plate subjected to convective heat transfer, such that the surface heat flux, the hot-gas temperture, and the gas heat transfer coefficient can be determined. It is shown that if the transient temperature measurement is made at a particular point located nearly midway in the thickness of the plate there is an important simplification in the data analysis process, in that the factor relating the surface heat flux to the measured rate of rise of temperature becomes invariant for a Fourier Number above 0.60 and for all values of the Biot Number. Parameters are derived, tabulated, and plotted which enable straightforward determination of the surface heat flux, the hot-gas temperature, of the plate, the rate of rise of temperature, the plate thickness and curvature, and the mean thermal properties of the plate material at the test temperature.
Document ID
19740004463
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Powell, W. B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
JPL-TR-32-1588
NASA-CR-136226
Report Number: JPL-TR-32-1588
Report Number: NASA-CR-136226
Accession Number
74N12576
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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