References 1 Mur thy , V.S. and Rose, W.C., Shear Stress Measurements in a Shock-Wave Boundary-Layer Interaction, AlAA Journal, Vol. 16, July 1978, pp. 667-672. 2 Baldwin, B.S. and Rose, W.C., Calculations of Shock Separation Boundary Layers, Proceedings of Conference on Aerodynamic Analysis Requiring Advanced Computers, Langley Research Center, March 1976, pp. 401-411. 3 Baldwin, B.S. and MacCormack, R.W., Modifications of the Law of the Wall and Algebraic Turbulence Modelling for Separated Boundary Layers, AIAA Paper 76-350, San Diego, Calif. , 1976. Johnson, C.B. and Kaufman, L.G., II, Interference Heating from Interactions of Shock Waves with Boundary Layers at Mach6, NASATN D-7649, Sept. 1974. 5 Tru i t t , R.W., Fundamentals of Aerodynamic Heating, Ronald Press, New York, 1960, pp. 222-223. Van Driest, E.R., Turbulent Boundary Layer in Compressible Fluids, Journal of Aeronautical Sciences, Vol. 18, Mar. 1951, pp. 145-160,216. Settles, G.S., Vas, I .E., and Bogdonoff, S.M., Details of a Shock-Separated Boundary Layer at a Compression Corner, AIAA Journal, Vol. 14, Dec. 1976, pp. 1709-1715. Reply by Authors to R.D. Kirchner