g, C.-M., Comment on 'Critique of Turbulence Models for Shock-Induced plow Separation,' AIAA Journal, Vol. 29, 1991. Ericsson, L. E., Critique of Turbulence Models for ShockInduced Flow Separation, AIAA Journal, Vol. 27, Nov. 1989, pp. 1648-1650. Hung, C. M., Computation of Three-Dimensional Shock Wave and Boundary-Layer Interactions, NASA TM 86780, August 1985. Dolling, D. S., Comparison of Sharp and Blunt Fin-Induced Shock Wave/Turbulent Boundary-Layer Interactions, AIAA Journal, Vol. 20, Oct. 1982, pp. 1385-1391. Knight, D., Horstman, C. C., Ruderich, R., Mao, M.-F., and Bogcjonoff, S. M., Supersonic Turbulent Flow Past a 3-D Swept Compression Corner at Mach 3, AIAA Paper 87-0551, Jan. 1987. Knight, D., Raufer, D., Horstman, C. C., and Bogdonoff, S. M., Supersonic Turbulent Flow Past a Swept Compression Corner, AIAA Paper 88-0310, Jan. 1988. Horstman, C. C., Prediction of Secondary Separation in Shock Wave Boundary-Layer Interactions, Computers and Fluids, Vol. 17, Nov. 4, 1989, pp. 611-614. Bogdonoff, S. M., AIAA Paper 90-0766, Jan. 1990. After some elaborate manipulation, Kim and Chung obtained an expression for the eddy viscosity vt: