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An Analysis of Exact and Approximate Equations for the Temperature Distribution in an Insulated Thick Skin Subjected to Aerodynamic HeatingThe problem of calculating the temperature distribution in an insulated slab is investigated. Exact and approximate solutions are obtained, and the results are compared to determine the ranges of applicability of the approximations. The approximations are found to be within 5 percent of the exact solution when the ratio of the thermal capacitance of the metal to that of the insulation and the ratio of the conductance of the metal to that of the insulation are sufficiently large. The roots of the characteristic equation of the exact solution are generally applicable to the two-slab heat-transfer problem and are tabulated up to the first nine roots.
Document ID
20010125633
Acquisition Source
Headquarters
Document Type
Other
Authors
Harris, Robert S., Jr.
(NASA Langley Research Center Hampton, VA United States)
Davidson, John R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
L-721
Report Number: L-721
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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