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Volumn 26, Issue 16, 2006, Pages 1771-1779

Combustion and cooling performance in an aero-engine annular combustor

Author keywords

Aero engine; CFD simulation; Combustor; Film cooling; Flow field

Indexed keywords

AIRCRAFT ENGINES; COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; COOLING; JETS;

EID: 33746806269     PISSN: 13594311     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.applthermaleng.2005.11.023     Document Type: Review
Times cited : (45)

References (18)
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    • V. Smililjanovski, N. Brehm, CFD liquid spray combustion analysis of a single annular gas turbine combustor, ASME Paper 99-GT-0300, 1999.
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    • R.E. Malecki, C.M. Rhie, R.G. McKinney, Application of an advanced CFD-based analysis system to the pw6000 combustor to optimize exit temperature distribution-Part I: description and validation of the analysis tool, ASME Paper 2001-GT-0062, 2001.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.