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Computation of nonlinear normal modes of large structures: application to a full-scale aircraft

  • M. Peeters
  • , Ludovic Renson
  • , Gaetan Kerschen
  • , J.-C. Golinval
  • , C. Stephan
  • , P. Lubrina

    Research output: Contribution to conference › Conference Abstract › peer-review

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    Abstract

    The objective of this paper is to demonstrate that the numerical computation of the nonlinear normal modes (NNMs) of complex real-world structures is now within reach. The application considered in this study is the airframe of the Morane-Saulnier Paris aircraft, whose ground vibration tests exhibited some nonlinear structural behaviors. The NNMs are computed using a numerical algorithm combining shooting and pseudo-arclength continuation.
    Original languageEnglish
    Publication statusUnpublished - 29 Jul 2011
    Event7th European Nonlinear Oscillation Conference (2011) - Rome, Italy
    Duration: 24 Jul 2011 → 29 Jul 2011
    Conference number: 7

    Conference

    Conference7th European Nonlinear Oscillation Conference (2011)
    Abbreviated titleENOC7
    Country/TerritoryItaly
    CityRome
    Period24/07/11 → 29/07/11

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