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Volumn , Issue , 2001, Pages

Numerical simulation of gas turbine swirl-stabilized injector dynamics

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; LARGE EDDY SIMULATION; MESSAGE PASSING; PARALLEL ARCHITECTURES; VORTEX FLOW;

EID: 85086614959     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-334     Document Type: Conference Paper
Times cited : (5)

References (4)
  • 4
    • 84897854334 scopus 로고    scopus 로고
    • An Experimental Study of Combustor Air Swirler Acoustic and Fluid Dynamic Sensitivities
    • presented at, Cleveland, OH, October 1-2
    • th Symposium on Propulsion, Cleveland, OH, October 1-2, 1997.
    • (1997) th Symposium on Propulsion
    • Cohen, J.1    Hibshman, J.R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.