Parametric study of simplex fuel nozzle internal flow and performance

AIAA journal

Volumn 38, Issue 7, 2000, Pages 1214-1218

  Sakman, A T ^a,f   Jog, M A ^b,c   Jeng, S M ^d   Benjamin, M A ^e  

^a UNIVERSITY OF CINCINNATI   (United States)

^b PARKER HANNIFIN CORPORATION   (United States)

^c ACRI   (United States)

^d and Nuclear Engineering

^e Department of Aerospace Engineering and Engineering Mechanics ^*

^f Gas Turbine Fuel Systems Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FUELS; ATOMIZERS; COMBUSTION CHAMBERS; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; GAS ENGINES; MATHEMATICAL MODELS; NOZZLES; ORIFICES; SWIRLING FLOW;

ADAPTIVE GRID GENERATION SCHEME; DISCHARGE COEFFICIENT; SIMPLEX FUEL NOZZLES; SPRAY CONE ANGLE; SWIRL CHAMBER;

AIRCRAFT ENGINES;

EID: 0034224998     PISSN: 00011452     EISSN: None     Source Type: None    
DOI: 10.2514/2.1090     Document Type: Article

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