An advanced spray model for application to the prediction of gas turbine combustor flow fields

Numerical Heat Transfer; Part A: Applications

Volumn 38, Issue 4, 2000, Pages 325-340

  Tolpadi, Anil K ^a   Aggarwal, Suresh K ^b   Mongia, Hukam C ^c  

^a GE GLOBAL RESEARCH   (United States)

^b 1120 Science and Engineering Offices   (United States)

^c GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 1842845276     PISSN: 10407782     EISSN: 15210634     Source Type: Journal    
DOI: 10.1080/104077800750022494     Document Type: Article

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