NASA NTRS · 19680000376
One-dimensional two-phase reacting gas nonequilibrium performance program
Abstract
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.
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Cherry, S. S., Frey, H. M., Kliegel, J. R., Quan, V.. 1968-10-01. One-dimensional two-phase reacting gas nonequilibrium performance program. https://ntrs.nasa.gov/citations/19680000376
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