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Volumn 5 PART B, Issue , 2006, Pages 961-971

Forced response variation of aerodynamically and structurally mistuned turbo-machinery rotors

Author keywords

[No Author keywords available]

Indexed keywords

AERO ELASTICITY CODE; BLADED DISC; CIVIL AERO ENGINE FAN; NAVIER STOKES AERO ELASTICITY CODE;

EID: 33750834192     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90948     Document Type: Conference Paper
Times cited : (13)

References (22)
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    • Whitehead, D.1
  • 2
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    • The effect of detuning upon the forced vibration of bladed disks
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  • 3
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  • 4
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    • Forced response of mistuned bladed discs using reduced-order modelling
    • Kruse, M., and Pierre, C., 1996. "Forced response of mistuned bladed discs using reduced-order modelling". AIAA.
    • (1996) AIAA
    • Kruse, M.1    Pierre, C.2
  • 5
    • 0036667030 scopus 로고    scopus 로고
    • A new method for dynamic analysis of mistuned bladed discs based in exact relationship between tuned and mistuned systems
    • July
    • Petrov, E., Sanliturk, K., and Ewins, D., 2002. "A new method for dynamic analysis of mistuned bladed discs based in exact relationship between tuned and mistuned systems". Trans. ASME Journal of Engineering for Gas Turbines and Power, 122, July, pp. 586-597.
    • (2002) Trans. ASME Journal of Engineering for Gas Turbines and Power , vol.122 , pp. 586-597
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  • 6
    • 0348226379 scopus 로고    scopus 로고
    • Mistuning identification of bladed discs using a fundamental mistuning model - Theory and application
    • Feiner, D., and Grifin, J., 2003. "Mistuning identification of bladed discs using a fundamental mistuning model - theory and application". ASME Journal of Turbomachinery, 126(1).
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    • Feiner, D.1    Grifin, J.2
  • 7
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    • Application of reducad-order aerodynamic modeling to the analysis of structural uncertainty in bladed disks
    • June
    • Willcox, K., and Peraire, J., 2002. "Application of reducad-order aerodynamic modeling to the analysis of structural uncertainty in bladed disks". Proceedings of ASME Turbo Expo 2002, Amsterdam, The Netherlands, June.
    • (2002) Proceedings of ASME Turbo Expo 2002, Amsterdam, the Netherlands
    • Willcox, K.1    Peraire, J.2
  • 9
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    • Investigation of the influence of aerodynamic coupling on response levels of mistuned bladed discs with weak structural coupling
    • (GT2005-69050), June
    • Sladojevic, I., Petrov, E., Sayma, A., Imregun, M., and Green, J., 2005. "Investigation of the influence of aerodynamic coupling on response levels of mistuned bladed discs with weak structural coupling". Proceedings of ASME Turbo Expo 2005, Reno, NY, USA(GT2005-69050), June.
    • (2005) Proceedings of ASME Turbo Expo 2005, Reno, NY, USA
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  • 10
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    • Coupled bending-bending-torsion flutter of a mistuned cascade with nonuniform blades
    • Tech. rep., Lewis Research Center. Cleverland, Ohio, USA
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    • Kaza, K.1    Kielb, R.2
  • 12
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  • 13
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  • 14
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    • Jan.
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  • 16
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    • June
    • Sayma, A., Vahdati, M., Sbardella, L., and Imregun, M., 2000. "Modeling of three-dimensional viscous compressible turbomachinery flows using unstructures hybrid grids". AIAA Journal, 38(6), June, pp. 945-954.
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  • 19
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  • 20
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  • 22
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.