Thermal degradation kinetics and surface pyrolysis of vinyl polymers
01 Nov 1970-AIAA Journal (American Institute of Aeronautics and Astronautics (AIAA))-Vol. 8, Iss: 11, pp 1989-1996
TL;DR: Cresci et al. as mentioned in this paper investigated the effect of Laminar, Transitional, and Turbulent Heat Transfer on Blunt-Nosed Bodies in Hypersonic Flow.
Abstract: Atmosphere," Izvestiya Akademii Nauk SSSR, Otdelenie Tekhnicheskikh Nauk, Mekhanika i Mashinostroenie, No. 4, 1965, pp. 36-40. 7 Benjamin, A. S., "The Effect of Albative Geometry Change on the Heating and Recession Characteristics of Sphere-Cones," AIAA Paper 66-992, Boston, Mass., 1966. 8 Cresci, R. J., MacKenzie, D. A., and Libby, P. A., "An Investigation of Laminar, Transitional, and Turbulent Heat Transfer on Blunt-Nosed Bodies in Hypersonic Flow," Journal of the Aerospace Sciences, Vol. 27, No. 6, June 1960, pp. 401-414. 9 Schlichting, H., Boundary Layer Theory, McGraw-Hill, New York, 1955, pp. 447-449. 10 Dippree, D. F. and Sabersky, R. H., "Heat and Momentum Transfer in Smooth and Rough Tubes at Various Prandtl Numbers," International Journal of Heat and Mass Transfer, Vol. 6, No. 5, May 1963, pp. 329-353. 11 Ames Research Staff, "Equations, Tables, and Charts for Compressible Flow," Rept. 1135, 1953, NACA. 12 Dunlap, R. and Kuethe, A. M., "Effects of Cooling on Boundary Layer Transition on a Hemisphere in Simulated Hypersonic Flow," Journal of the Aerospace Sciences, Vol. 29, No. 12, Dec. 1962, pp. 145^1461. 13 Fay, J. A. and Riddell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," Journal of the Aerospace Sciences, Vol. 25, No. 2, Feb. 1958, pp. 73-85. 14 Sutton, G. W., "On the Stable Shape of a Slender Ablating Graphite Body," Journal of the Aerospace Sciences, Vol. 26, No. 10, Oct. 1959, pp. 681-682.
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