Chemical species and chemical reactions of importance in nonequilibrium rocket engine performance calculations.
Chemical species and reactions determined for propellants in calculating nonequilibrium rocket engine performance
Gold, P. I.↗
Engineering topics
Kliegel, J. R.
Publications and source records attributed to Kliegel, J. R..
Axisymmetric two-phase perfect gas performance program
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.
Kliegel, J. R.↗
One-dimensional reacting gas nonequilibrium performance program
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.
Frey, H. M.↗
One-dimensional two-phase reacting gas nonequilibrium performance program
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.
Cherry, S. S.↗
Axisymmetric reacting gas nonequilibrium performance program
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.
Kliegel, J. R.↗
Kinetic performance of barrier-cooled rocket nozzles.
Flow of chemically reacting propellant exhaust mixture in barrier cooled axisymmetric rocket nozzle
Frey, H. M.↗
Convergent-divergent nozzle flows.
Convergent-divergent nozzle flow field solution obtained in form of perturbation about one dimensional flow field
Kliegel, J. R.↗
Axisymmetric two-phase reacting gas nonequilibrium nozzle flows analysis
Computer program for axisymmetric two-phase reacting gas nonequilibrium nozzle flows analysis
Kliegel, J. R.↗
Convergent-divergent nozzle flows
Uniform two-zone perfect gas expansions in convergent-divergent nozzles
CONVERGENT-DIVERGENT NOZZLE↗
One-dimensional reacting gas nonequilibrium performance program Interim analysis report
Computer program for calculating inviscid one- dimensional nonequilibrium nozzle expansion of propellant exhaust mixtures containing C, H, O, N, F, and Cl
ONE-DIMENSIONAL FLOW↗