Reduced order model of a multistage bladed rotor with geometric mistuning via modal analyses of finite element sectors

Yasharth Bhartiya, Alok Sinha

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    1 Scopus citations

    Abstract

    An algorithm to generate a reduced order model of a multi-stage rotor in which each stage has a different number of blades has been developed. It is shown that a reduced order model can be developed on the basis of tuned modes of certain bladed disks which can be easily obtained via sector analyses. Further, it is shown that reduced order model can also be obtained when blades are geometrically mistuned. This algorithm is similar to the modified modal domain analysis, which has been recently developed for a single-stage bladed rotor with geometric mistuning. The validity of this algorithm is shown for the finite element model of a two-stage bladed rotor. In addition, the statistical distributions of peak maximum amplitudes and natural frequencies of a two-stage rotor are generated via Monte Carlo simulations for different patterns of geometric mistuning.

    Original languageEnglish (US)
    Title of host publicationASME Turbo Expo 2010
    Subtitle of host publicationPower for Land, Sea, and Air, GT 2010
    Pages939-948
    Number of pages10
    Volume6
    EditionPARTS A AND B
    DOIs
    StatePublished - Dec 1 2010
    EventASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 - Glasgow, United Kingdom
    Duration: Jun 14 2010Jun 18 2010

    Other

    OtherASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
    CountryUnited Kingdom
    CityGlasgow
    Period6/14/106/18/10

    All Science Journal Classification (ASJC) codes

    • Engineering(all)

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