A NEW APPROACH TO NONEQUILIBRIUM STATISTICAL MECHANICS OF GASES
Gas dynamics - nonequilibrium statistical mechanics
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Gas dynamics - nonequilibrium statistical mechanics
Shock-tube studies of the supersonic nozzle expansion of diatomic gases, to analyze vibrational and dissociative nonequilibrium
Influence of catalyst on the atomic recombination in nonequilibrium nozzle flows of hydrogen
Shallow angle flight paths of high speed reentry vehicles necessitates analysis of the factors controlling the rate of convective heating and the effect of nonequilibrium flow
Spectroscopic method for taking nonequilibrium shock front rotational, vibrational, and electronic temperature measurements in relaxation zone
Computer program for calculating inviscid one-dimensional equilibrium, frozen and nonequilibrium nozzle expansion of propellant exhaust mixtures
Vibration-dissociation coupling models for nonequilibrium hypersonic flow field past wedge
Gas dynamics in nonequilibrium two-step rocket nozzle design
Steady state composition of low density nonequilibrium hydrogen plasma
Martian entry condition analyzed as nonequilibrium flow field phenomenon, noting chemical kinetics and radiation behind shock wave in gas mixtures
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of gaseous propellant exhaust mixtures containing the elements - carbon, hydrogen, oxygen, nitrogen, fluorine and chlorine. The program performs calculations for conical nozzles only.
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing carbon, hydrogen, oxygen, nitrogen, fluorine, chlorine and either aluminum, beryllium, boron or lithium. This program performs calculations for conical nozzles only.
Computer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing these six elements - carbon, hydrogen, oxygen, nitrogen, fluorine, and chlorine plus either aluminum, beryllium, boron or lithium. This program will perform calculations for contoured and conical nozzles.
Approximate solution of turbulent boundary layer on plane catalytic surfaces in nonequilibrium dissociating gas environments
One dimensional analysis of magnetoplasm dynamic arcs with nonequilibrium ionization
Differential approximations used to determine effects of nongray gas behavior and nonequilibrium ionization in radiating hypersonic shock layers
Hydrodynamic equations for calculating nonisentropic nonequilibrium gas flow through nozzle induced by friction and heat exchange
Solution of Boltzmann, and rate equations for bound electronic states in nonequilibrium magnetohydrodynamic plasma