Abstract

Turbulent Boundary Layer on a Smooth Flat Plate With and Without Heat Transfer, Journal of Fluid Mechanics, Vol. 18, Pt. 1, Jan. 1964, pp. 117-143. * Reshotko, E. and Tucker, M., Approximate of the Compressible Turbulent Boundary Layer With Heat Transfer and Arbitrary Pressure Gradient, TN 4154, 1957, NACA. 12 Dhawan, S. and Narasimha, R., Some Properties of Boundary Layer Flow During the Transition From Laminar to Turbulent Motion, Journal of Fluid Mechanics, Vol. 3, No. 4, April 1958, pp. 418-436. 13 Maslen, S. H., Inviscid Hypersonic Flow Past Smooth Symmetric Bodies, AIAA Journal, Vol. 2, No. 6, June, 1964, pp. 1055-1061. 14 Maslen, S. H., Asymmetric Hypersonic Flow, CR-2123, Sept. 1972, NASA. 15 DeJarnette, F. R., Calculation of Heat Transfer on ShuttleType Configurations Including the of Variable Entropy at Boundary Layer Edge, CR-112180, Oct. 1972, NASA. 16 Hopkins, E. J. and Inouye, M., An Evaluation of Theories for Predicting Turbulent Skin Friction and Heat Transfer on Flat Plates at Supersonic and Hypersonic Mach Numbers, AIAA Journal, Vol. 9, No. 6, June, 1971, pp. 993-1003. 17 Cleary, J. W., Effects of Angle of Attack and Bluntness on Laminar Heating-Rate Distributions of a 15° Cone at a Mach Number of 10.6, TN D-5450, 1969, NASA. 18 Hillsamer, M. E., and Rhudy, J. P., Heat-Transfer and Shadowgraph Tests of Several Elliptical Lifting Bodies at Mach 10, U.S. Air Force, AEDC-TDR-64-19,1964, Arnold Engineering Development Center, Tullahoma, Tenn.

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