Abstract
References Baldwin, B. S., and Lomax, H., Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow, AIAA Paper 78-257, Jan. 1978. Chien, K. Y, Predictions of Channel and Boundary Layer Flows with a Low Reynolds Number Turbulence Model, AIAA Journal, Vol. 20, No. 1, 1982, pp. 33-38. Baysal, O., and Hoffman, W. B., Simulation of Three-Dimensional Shear Flow Around a Nozzle-Afterbody at High Speeds, Journal of Fluids Engineering, Vol. 114, June 1992, pp. 178-185. ^Launder, B. E., and Priddin, C. H., A Comparison of Some Proposals for the Mixing Length Near a Wall, International Journal of Heat and Mass Transfer, Vol. 16, No. 3,1973, pp. 700-702. Nichols, R. H., A Two-Equation Model for Compressible Flows, AIAA Paper 90-0494, Jan. 1990. Hu, J., and Rizzi, A., Assessment of Compressibility and PressureGradient Corrections for Modeling Turbulent Hypersonic Nozzle Flows AIAA Paper 95-2313, June 1995. Rizzi, A., Eliasson, P., Lindblad, I., Hirsch, Ch., Lacor, C., and Haeuser, J., The Engineering of Multiblock/Multigrid Software for NavierStokes Flows on Structured Meshes, Computers and Fluids, Vol. 22, No. 2/3,1993, pp. 341-367. Hovstadius, G., Measurement of Boundary Layer Properties in Two Hypersonic Nozzles, Aeronautical Research Inst. of Sweden, FFA Rept. AU-624, Stockholm, Sweden, May 1971.
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