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Experimental and Theoretical Study of Heat Conduction for Air up to 5000 KThe theoretical value of the integral of thermal conductivity is compared with the experimental values from shock-tube measurements. The particular case considered is the one-dimensional nonsteady flow of heat through air at constant pressure. This approach has been previously described in NASA TR R-27. experiment was uncertain because of the large scatter in the experimental data. In this paper, an attempt is made to improve the correlation by use of a more refined calculation of the integral of thermal conductivity, and by use of improved experimental techniques and instrumentation. As a result of these changes, a much closer correlation is shown between the experimental and theoretical heat-flux potentials. This indicates that the predicted values of the coefficient of thermal conductivity for high-temperature air may be suitably accurate for many engineering needs, up to the limits of the test (4600 K).
Document ID
20040006305
Acquisition Source
Ames Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Peng, Tzy-Cheng
(NASA Ames Research Center Moffett Field, CA, United States)
Ahtye, Warren F.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 21, 2013
Publication Date
February 1, 1961
Subject Category
Meteorology And Climatology
Report/Patent Number
NASA-TN-D-687
A-401
Report Number: NASA-TN-D-687
Report Number: A-401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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