Efficient Computation of "Stiff" Chemically Reacting Flow in Turbulent Free Jets
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[1] D. Jensen,et al. Prediction of rocket exhaust flame properties , 1975 .
[2] A. C. Victor. Calculations of rocket plume afterburning coupled to reacting base recirculation regions , 1977 .
[3] R. D. Richtmyer,et al. Difference methods for initial-value problems , 1959 .
[4] T. Teichmann,et al. Introduction to physical gas dynamics , 1965 .
[5] H. E. Bailey,et al. A critical analysis of various numerical integration methods for computing the flow of a gas in chemical nonequilibrium , 1967 .
[6] H. Pergament,et al. Influence of Chemical Kinetic and Turbulent Transport Coefficients on Afterburning Rocket Plumes , 1971 .
[7] R. Maccormack. The Effect of Viscosity in Hypervelocity Impact Cratering , 1969 .
[8] S. Lee,et al. Analysis of coaxial free mixing using the turbulent kinetic energy method , 1971 .
[9] D. B. Spalding,et al. A finite-difference procedure for solving the equations of the two-dimensional boundary layer , 1967 .
[10] P. D. Thomas,et al. Numerical Solution for Three-Dimensional Inviscid Supersonic Flow , 1972 .
[11] S. C. Lee,et al. Use of turbulent kinetic energy in free mixing studies , 1970 .
[12] H. S. Pergament,et al. Fast Computer Program for Nonequilibrium Rocket Plume Predictions , 1972 .