NASA NTRS · 19680000374
Axisymmetric two-phase perfect gas performance program
Abstract
Computer program calculates the inviscid axisymmetric nozzle expansion of propellant systems having both gaseous and condensed exhaust products. The program uses velocity and thermal lags and will perform calculations for contoured and conical nozzles.
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Kliegel, J. R., Nickerson, G. R.. 1968-10-01. Axisymmetric two-phase perfect gas performance program. https://ntrs.nasa.gov/citations/19680000374
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