Numerical simulation of C-H-O-N system liquid rocket engine nozzle flow

Tuijin Jishu/Journal of Propulsion Technology

Volumn 23, Issue 5, 2002, Pages 391-393

  Cai, Guo Biao ^a   Ma, Zhao Kai ^a   Zhang, Hua Zhao ^b  

^a BEIHANG UNIVERSITY   (China)

^b Beijing Institute of Space System Engineering   (China)

Author keywords

Engine nozzle; Flow distribution; Liquid propellant rocket engine; Nozzle flow; Numerical simulation; Reaction kinetics

Indexed keywords

COMPUTER SIMULATION; LIQUID PROPELLANTS; NOZZLES; VISCOUS FLOW;

ENGINE NOZZLE FLOW; FLOW FIELD DISTRIBUTION; LIQUID PROPELLANT ROCKET ENGINE; NUMERICAL SIMULATION; REACTION KINETICS;

ROCKET ENGINES;

EID: 0036820023     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Drummond J P, Rongers R C, Hussaini M Y. A Detailed numerical model of supersonic reacting mixing layer[R]. AIAA 86-1427.
2. John S Evans, Charles J Schexnayder Jr. Influence of chemical kinetics and unmixedness on burning in supersonic hydrogen flames[J]. AIAA Journal, 1980, 18(2).
3. Charles K Westbrook, Frederick L Dryer. Chemical kinetic modeling of hydrocarbon combustion[J]. Prog. Energy Combus. Sci, 1984, 10.