Simulation of Convective and Radiative Entry Heating, Advances in Hypervelocity Techniques, edited by A. M. Krill, Plenum, New York, 1962. 5 Marvin, J. G. and Pope, R. B., Laminar Convective Heating and Ablation in the Mars Atmosphere, AIAA Journal, Vol. 5, No. 2, Feb. 1967, pp. 240-248. 6 Wilson, G. R. (compiler), Thermophysical Properties of Six Charring Ablators from 140° to 700 °K and Two Chars from 800° to 3000°K, TN D-2991, Oct. 1965, NASA. 7 Parker, J. A., Needs for Characterization and Process Control of Low-Density Composites for Aerospace Application, presented at International Society of Plastics Institute, New York, June 1966. 8 Vojvodich, N. S. and Pope, R. B., /The Influence of Ablation on Stagnation Region Convective Heating for Dissociated and Partially Ionized Boundary Layer Flows, Proceedings of the 1965 Heat Transfer and Fluid Mechanics Institute, edited by A. F. Charwat et al., Stanford University Press, Stanford, Calif., 1965. 9 Pope, R. B., Stagnation-Point Convective Heat Transfer in Frozen Boundary Layers, Paper 68-15, Jan. 1968, AIAA. 10 Scala, S. M. and Gilbert, L. M., Sublimation of Graphite at Hypersonic Speeds, AIAA Journal, Vol. 3, No. 9, Sept. 1965, pp. 1635-1644. 11 Wakefield, R. M., Lundell, J. H., and Dickey, R. R., The Effect of Oxygen Depletion in Gas-Phase Chemical Reactions on the Surface Recession of Charring Ablators, Paper 68-302, April 1968, AIAA. 12 Emmons, H. W. and Leigh, D., Tabulation of the Blasius Function with Blowing and Suction, Combustion Aerodynamics Lab. Interim TR9 Nov. 1953, Div. of Applied Science, Harvard Univ.
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