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Volumn 4, Issue , 2000, Pages

Prediction of low engine order inlet distortion driven resonance in a low aspect ratio fan

Author keywords

[No Author keywords available]

Indexed keywords

DATA HANDLING; ENGINES; FORECASTING; NAVIER STOKES EQUATIONS; RESONANCE; STRUCTURAL DYNAMICS;

EID: 84955301035     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0374     Document Type: Conference Paper
Times cited : (9)

References (12)
  • 2
    • 84955295454 scopus 로고    scopus 로고
    • An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion
    • Paper proposed for
    • Bréard, C., Vahdati, M., Sayma, A.I. and Imregun, M., 2000. An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion. Paper proposed for ASME Gas Turbine Expo.
    • (2000) ASME Gas Turbine Expo
    • Bréard, C.1    Vahdati, M.2    Sayma, A.I.3    Imregun, M.4
  • 4
    • 0026765731 scopus 로고
    • The calculation of 3 dimensional viscous flow through multistage turbomachines
    • Denton, J.D., 1992. The calculation of 3 dimensional viscous flow through multistage turbomachines. ASME J. Turbomachinery, 114, No 1.
    • (1992) ASME J. Turbomachinery , vol.114 , Issue.1
    • Denton, J.D.1
  • 6
    • 84925988315 scopus 로고
    • An approach for multi-stage calculations incorporating unsteadiness
    • Giles, M.B., 1992. An approach for multi-stage calculations incorporating unsteadiness. ASME paper 92-GT-282.
    • (1992) ASME Paper 92-GT-282
    • Giles, M.B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.