NASA NTRS · 19680000377
Axisymmetric reacting gas nonequilibrium performance program
Abstract
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.
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Kliegel, J. R., Melde, J. E., Nickerson, G. R., Quan, V.. 1968-10-01. Axisymmetric reacting gas nonequilibrium performance program. https://ntrs.nasa.gov/citations/19680000377
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