Simulation of unsteady flows in an axisymmetric research combustor using detailed-chemical kinetics

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Katta, Viswanath R ^a   Roquemore, W M ^b  

^a INNOVATIVE SCIENTIFIC SOLUTIONS INC   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR ENTRAINMENT; CODES (SYMBOLS); COMBUSTION; COMBUSTORS; COMPUTATIONAL CHEMISTRY; COMPUTATIONAL FLUID DYNAMICS; DIRECT INJECTION; GAS DYNAMICS; LOCKS (FASTENERS); PROPULSION; UNSTEADY FLOW; VORTEX FLOW;

CHEMISTRY MECHANISM; DETAILED CHEMICAL KINETIC; DYNAMIC CHARACTERISTICS; PERFORMANCE CHARACTERISTICS; PROPANE COMBUSTION; RESEARCH COMBUSTORS; REVERSIBLE REACTION; TRAPPED VORTEX COMBUSTOR;

STRAIN RATE;

EID: 85085407380     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3766     Document Type: Conference Paper

References (16)

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