Mixing of multiple jets with a confined subsonic crossflow Part II - Opposed rows of orifices in rectangular ducts

Proceedings of the ASME Turbo Expo

Volumn 2, Issue , 1997, Pages

  Holdeman, James D ^a   Liscinsky, David S ^b   Bain, Daniel B ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^c CFD RESEARCH CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; ALTERNATIVE FUELS; COAL COMBUSTION; COMBUSTION CHAMBERS; DUCTS; GAS TURBINES; MASS TRANSFER; MIXING; MOMENTUM; ORIFICES;

COMPUTATIONAL RESULTS; CROSS SECTIONAL AREA; GEOMETRIC VARIABLES; GEOMETRIC VARIATIONS; MASS FLOW RATIOS; MOMENTUM FLUX RATIOS; RECTANGULAR DUCTS; THREE-DIMENSIONAL FLOW;

FIGHTER AIRCRAFT;

EID: 84973594863     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-439     Document Type: Conference Paper

References (36)

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