OPTIMIZATION METHOD FOR THE DETERMINATION OF THE IMPORTANT FLUTTER MODES.

E. 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

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