OPTIMIZATION METHOD FOR THE DETERMINATION OF THE IMPORTANT FLUTTER MODES.

Eliahu Nissim, I. Lottati

    Research output: Contribution to journalConference articlepeer-review

    Abstract

    An optimization method for the determination of the dominant flutter modes is presented in this paper. The method is based on minimization of quadratic values of subdeterminants derived from the equations of motion. The effectiveness of the method is illustrated by seven numerical examples.

    Original languageEnglish
    Pages (from-to)741-747
    Number of pages7
    JournalCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
    DOIs
    StatePublished - 1980
    EventCollect Tech Pap AIAA ASME ASCE AHS Struct Struct Dyn Mater Conf 21st, Pt 2 - Seattle, WA, USA
    Duration: 12 May 198014 May 1980

    Fingerprint

    Dive into the research topics of 'OPTIMIZATION METHOD FOR THE DETERMINATION OF THE IMPORTANT FLUTTER MODES.'. Together they form a unique fingerprint.

    Cite this