INTERFACING NONEQUILIBRIUM MODELS WITH COMPUTATIONAL FLUID DYNAMICS METHODS

[1]  Xiaolin Zhong,et al.  Stabilization of the Burnett Equations and Application to Hypersonic Flows , 1993 .

[2]  A. Aguilar,et al.  Quasiclassical trajectory study of the N(4Su) + O2 (X 3Σ−g)→NO (X 2Π) + O (3Pg) atmospheric reaction on the 2A′ ground potential energy surface employing an analytical Sorbie—Murrell potential , 1993 .

[3]  Martin Karplus,et al.  Exchange Reactions with Activation Energy. I. Simple Barrier Potential for (H, H2) , 1965 .

[4]  G. Candler,et al.  An overlay method for calculating excited state species properties in hypersonic flows , 1995 .

[5]  G. Candler,et al.  Overlay method for calculating excited state species properties in hypersonic flows , 1997 .

[6]  Jong-Hun Lee,et al.  Basic governing equations for the flight regimes of aeroassisted orbital transfer vehicles , 1984 .

[7]  R. Jaffe,et al.  Calculated potential surfaces for the reactions: O+N2→NO+N and N+O2→NO+O , 1987 .

[8]  F. Mota,et al.  Dynamics of the N(4Su) + NO(X 2Π) → N2(X 1Σg+) + O(3Pg) atmospheric reaction on the 3A‘ ground potential energy surface. I. Analytical potential energy surface and preliminary quasiclassical trajectory calculations , 1992 .

[9]  G. Candler,et al.  Kinetics of the N2 + O yields NO + N reaction in nonequilibrium flows , 1996 .

[10]  L. Raff,et al.  Classical Trajectory Methods in Molecular Collisions , 1976 .

[11]  D. Burnett The Distribution of Molecular Velocities and the Mean Motion in a Non-Uniform Gas , 1936 .

[12]  E. Pollak,et al.  A quasiclassical trajectory study of the F+HH⇄FH+H reaction , 1983 .

[13]  S. Heims MOMENT EQUATIONS FOR VIBRATIONAL RELAXATION COUPLED WITH DISSOCIATION , 1963 .

[14]  Graham V. Candler,et al.  Examination of theory for bow shock ultraviolet rocket experiments. II , 1994 .

[15]  Chul Park,et al.  Assessment of a two-temperature kinetic model for dissociating and weakly ionizing nitrogen , 1986 .

[16]  Forrest E. Lumpkin,et al.  Accuracy of the Burnett equations for hypersonic real gas flows , 1991 .

[17]  Donald G. Truhlar,et al.  Reactive Scattering Cross Sections III: Quasiclassical and Semiclassical Methods , 1979 .

[18]  Graham V. Candler,et al.  Predicting failure of the continuum fluid equations in transitional hypersonic flows , 1994 .

[19]  Graham V. Candler,et al.  Review of Chemical-Kinetic Problems of Future NASA Missions, II: Mars Entries , 1993 .

[20]  A. Aguilar,et al.  Dynamics of the N(4Su)+NO(X 2Π)→N2(X 1Σ+g)+O(3Pg) atmospheric reaction on the 3A‘ ground potential energy surface. II. The effect of reagent translational, vibrational, and rotational energies , 1993 .

[21]  Graham V. Candler,et al.  Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles , 1993 .

[22]  D. M. Hirst Potential energy surfaces : molecular structure and reaction dynamics , 1985 .

[23]  Graham V. Candler,et al.  Dissociation modeling in low density hypersonic flows of air , 1995 .

[24]  Don L. Bunker,et al.  Classical Trajectory Methods , 1971 .

[25]  J. Muckerman,et al.  Importance sampling and histogrammic representations of reactivity functions and product distributions in Monte Carlo quasiclassical trajectory calculations , 1978 .

[26]  G. Candler,et al.  Experimental evaluation of vibration-dissociation coupling models , 1994 .

[27]  Sergey O. Macheret,et al.  Nonequilibrium dissociation rates behind strong shock waves: classical model , 1993 .

[28]  P. V. Marrone,et al.  Chemical Relaxation with Preferential Dissociation from Excited Vibrational Levels , 1963 .