Computational assessment of afterburning cessation mechanisms in fuel-rich rocket exhaust plumes

Journal of Propulsion and Power

Volumn 17, Issue 1, 2001, Pages 111-119

  Calhoon W , Jr ^a  

^a Syst Simulation Dvmt Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION; COMPUTER SIMULATION; EXHAUST GASES; FLAME RESEARCH; HEAT TRANSFER; NAVIER STOKES EQUATIONS; NOZZLES; REYNOLDS NUMBER; THERMAL PLUMES; TURBULENCE;

AFTERBURNING CESSATION MECHANISMS; CLASSICAL FLAME EXTINCTION MECHANISM; DAMKOHLER NUMBER EFFECT; FUEL RICH ROCKET EXHAUST PLUMES; GENERAL AERODYNAMIC SIMULATION PROGRAM; RELAMINARIZATION;

BOOSTERS (ROCKET);

EID: 0034823931     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5715     Document Type: Article

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