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Volumn 30 II, Issue , 2005, Pages 2893-2901

Effect of exhaust nozzle geometry on combustor flow field and combustion characteristics

Author keywords

Emissions; Exhaust nozzle contraction ratio; Gas turbine combustion; Swirling flow

Indexed keywords


EID: 33750688246     PISSN: 15407489     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1016/j.proci.2004.08.189     Document Type: Article
Times cited : (42)

References (17)
  • 9
    • 0015129209 scopus 로고
    • T. Sarpkaya, AIAA J. 9 (1971) 1792-1799.
    • (1971) AIAA J. , vol.9 , pp. 1792-1799
    • Sarpkaya, T.1
  • 14
    • 33750921844 scopus 로고
    • Department Report No. 102, Imperial College of Science and Technology Aeronautics
    • H.B. Squire, Department Report No. 102, Imperial College of Science and Technology Aeronautics, 1960.
    • (1960)
    • Squire, H.B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.