NASA NTRS · 19680000375
One-dimensional reacting gas nonequilibrium performance program
Abstract
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.
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Frey, H. M., Kliegel, J. R.. 1968-10-01. One-dimensional reacting gas nonequilibrium performance program. https://ntrs.nasa.gov/citations/19680000375
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