Effect of Reaction Mechanism in Shock-Induced Combustion Simulations
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[1] W. Shyy,et al. Evaluation of source term treatments for high-speed reacting flows , 1998 .
[2] James K. Clutter,et al. Computation of high-speed reacting flows , 1997 .
[3] R. J. Duchovic,et al. Conventional transition state theory/Rice–Ramsperger–Kassel–Marcus theory calculations of thermal termolecular rate coefficients for H(D)+O2+M , 1996 .
[4] Ten-See Wang,et al. Investigation of chemical kinetics integration algorithms for reacting flows , 1995 .
[5] P. M. Rubins,et al. Review of shock-induced supersonic combustion research and hypersonic applications , 1994 .
[6] Myles Sussman,et al. A computational study of unsteady shock-induced combustion of hydrogen-air mixtures , 1994 .
[7] Akiko Matsuo,et al. Numerical investigation of oscillatory instability in shock-induced combustion around a blunt body , 1993 .
[8] Huan-Min Shang,et al. Numerical analysis of complex internal and external viscous flows with a second-order pressure-based method , 1993 .
[9] Gregory J. Wilson,et al. Computation of unsteady shock-induced combustion using logarithmic species conservation equations , 1993 .
[10] Kozo Fujii,et al. Flow features of shock-induced combustion around projectile traveling at hypervelocities , 1993 .
[11] J. Ahuja,et al. Numerical simulation of shock-induced combustion in a superdetonative hydrogen-air system , 1993 .
[12] J. Shuen,et al. Upwind differencing and LU factorization for chemical non-equilibrium Navier-Stokes equations , 1992 .
[13] Graham V. Candler,et al. Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium , 1991 .
[14] Adam P. Bruckner,et al. Numerical simulation of hypervelocity projectiles in detonable gases , 1991 .
[15] Gregory J. Wilson,et al. Modeling supersonic combustion using a fully-implicit numerical method , 1990 .
[16] Meng-Sing Liou,et al. Splitting of inviscid fluxes for real gases , 1990 .
[17] Seung-Ho Lee,et al. Calculation of nonequilibrium hydrogen-air reactions with implicit flux vector splitting method , 1989 .
[18] H. C. Yee,et al. Semi-implicit and fully implicit shock-capturing methods for nonequilibrium flows , 1989 .
[19] C. Rhie,et al. Numerical analysis of reacting flows using finite rate chemistry models , 1989 .
[20] C. J. Jachimowski,et al. An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion , 1988 .
[21] R. C. Rogers,et al. A detailed numerical model of a supersonic reacting mixing layer , 1986 .
[22] J. Troe,et al. High-pressure falloff curves and specific rate constants for the reactions atomic hydrogen + molecular oxygen .dblharw. perhydroxyl .dblharw. hydroxyl + atomic oxygen , 1985 .
[23] R. Maccormack. Current status of numerical solutions of the Navier-Stokes equations , 1985 .
[24] S. Osher,et al. A new class of high accuracy TVD schemes for hyperbolic conservation laws. [Total Variation Diminishing] , 1985 .
[25] James C. Keck,et al. Laminar burning velocities in stoichiometric hydrogen and hydrogenhydrocarbon gas mixtures , 1984 .
[26] Jürgen Warnatz,et al. Concentration-, Pressure-, and Temperature-Dependence of the Flame Velocity in Hydrogen-Oxygen-Nitrogen Mixtures , 1981 .
[27] J. Steger,et al. Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods , 1981 .
[28] C. J. Schexnayder,et al. Influence of Chemical Kinetics and Unmixedness on Burning in Supersonic Hydrogen Flames , 1980 .
[29] G. Moretti. A new technique for the numerical analysis of nonequilibrium flows , 1965 .
[30] Kozo Fujii,et al. First damkohler parameter for prediction and classification of unsteady combustions around hypersonic projectiles , 1996 .
[31] K. Fujii,et al. Computational study of large-disturbance oscillations in unsteady supersonic combustion around projectiles , 1995 .
[32] Myles A. Sussman,et al. Source term evaluation for combustion modeling , 1993 .
[33] J. Philip Drummond,et al. Supersonic reacting internal flowfields , 1991 .
[34] Jürgen Troe,et al. Rate Coefficients of Thermal Dissociation, Isomerization, and Recombination Reactions , 1984 .
[35] J. Warnatz. Rate Coefficients in the C/H/O System , 1984 .
[36] M. W. Slack,et al. Rate coefficient for H + O2 + M = HO2 + M evaluated from shock tube measurements of induction times , 1977 .
[37] H. Lehr,et al. Experiments on Shock-Induced Combustion , 1972 .