Abstract
References ^Harris, H. J., A. Graphical Method for Obtaining the Transient Bondline Temperature for Two Finite Composite Slabs Subjected to Aerodynamic Heating, IOC 69.4352.8-22, Dec. 1969, TRW Systems Group, Houston, Texas. 2 Churchill, R. V., Operational Mathematics, McGraw-Hill, New York, 1958, pp. 38-40, 229-231. 3 Grover, J. H. and Holter, W. H., Solution of the Transient Heat-Conduction Equation for an Insulated, Infinite Metal Slab, Jet Propulsion, Vol. 27, No. 12, Dec. 1957, pp. 1249-1252. 4 Mayer, E., Flow in Composite Slabs, ARS Journal, Vol. 22, No. 3, May-June 1952, pp. 150-158. 5 Harris, R. S., Jr. and Davidson, J. R., An Analysis of Exact and Approximate Equations for the Temperature Distribution in an Insulated Thick Skin Subjected to Aerodynamic Heating, TN D-519, Jan. 1961, NASA. 6 Grover, J. H. and Holter, W. H., Insulation Temperature for the Transient Heating of an Insulated Infinite Metal Slab, Journal of the American Rocket Society, Vol. 30, No. 9, Sept. 1960, pp.907-908. 7 Schneider, P. J., Conduction Heat Transfer, Addison-Wesley, Reading, Mass., Sept. 1957, pp. 272-273, 235-236. 8 Abramowitz, M. and Stegun, I. A., Handbook of Mathematical Functions with Formulas, Graphs, and Mathematical Tables, National Bureau of Standards Applied Mathematics Series 55, June 1964, p. 225. 9 Derivation of Duhamel Method for Calculating Back Face Temperatures, General Dynamics Corp., Fort Worth, Texas, 1960.
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