Computation of nonequilibrium, supersonic three-dimensional inviscidflow over blunt-nosed bodies
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[1] De Jarnette. Two different interpretations of measured dissociation-rate constants and their effects on coupled vibrational-dissociational flows of oxygen over a wedge , 1967 .
[2] M. J. Lanfranco,et al. Results of a flight experiment on the catalytic efficiency of the Space Shuttle heat shield , 1982 .
[3] H. E. Bailey,et al. Reacting Nonequilibrium Flow around the Space Shuttle Using a Time-Split Method , 1975 .
[4] J. H. Spurk,et al. Characteristic calculation of flowfields with chemical reactions. , 1966 .
[5] C. E. Treanor,et al. A Method for the Numerical Integration of Coupled First-Order Differential Equations with Greatly Different Time Constants , 1966 .
[6] C. Kyriss. A time dependent solution for the blunt body flow of a chemically reacting gas mixture , 1970 .
[7] H. E. Bailey. Numerical Integration of the Equations Governing the One‐Dimensional Flow of a Chemically Reactive Gas , 1969 .
[8] C. Li. Time-Dependent Solutions of Nonequilibrium Airflow past a Blunt Body , 1972 .
[9] T. Teichmann,et al. Introduction to physical gas dynamics , 1965 .
[10] W. P. Crowley,et al. NUMERICAL ADVECTION EXPERIMENTS1 , 1968 .
[12] Joseph Hilsenrath,et al. TABLES OF THERMODYNAMIC PROPERTIES OF NITROGEN IN CHEMICAL EQUILIBRIUM INCLUDING SECOND VIRIAL CORRECTIONS FROM 2000 K TO 15,000 K , 1964 .
[13] M. J. Lighthill,et al. Dynamics of a dissociating gas Part I Equilibrium flow , 1957, Journal of Fluid Mechanics.
[14] H. E. Bailey,et al. A critical analysis of various numerical integration methods for computing the flow of a gas in chemical nonequilibrium , 1967 .