Computer program for the numerical solution of nonequilibrium expansions of reacting gas mixtures
Computer program for numerical solution of reacting gas mixture nonequilibrium expansions
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Computer program for numerical solution of reacting gas mixture nonequilibrium expansions
Chemical species and reactions of propellant systems determined for nonequilibrium flow - Performance calculations
Nonequilibrium ionization in asymmetric plasma sheath determined for Apollo spacecraft at superorbital velocity reentry
Simplified model of segmented electrode losses in nonequilibrium magnetohydrodynamic generators
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Centered one-dimensional unsteady expansion calculated for reacting gas mixture subject to vibrational and chemical nonequilibrium
Equation for sonic line in nonequilibrium nozzle flows of gas and application in supersonic flow computations
Hypersonic nonequilibrium flow at reentry of space vehicles and thermodynamic relations
Numerical integration methods for computing flow of gas in chemical nonequilibrium behind normal shock wave
Nonequilibrium radiation and ionization in shock waves
Dissociational rate constants and vibrational relaxation times modifications, considering coupling of vibrational and dissociational nonequilibrium of expanding gas in nozzle
Simple model atom selection for electron density calculation in low temperature nonequilibrium Cs plasmas
This paper represents an on-going effort at NASA Ames Research Center to develop a physics-based nonequilibrium model for hypersonic entry into the Martian atmosphere.