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.
|Number of pages
|Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
|Published - 1980
|Collect Tech Pap AIAA ASME ASCE AHS Struct Struct Dyn Mater Conf 21st, Pt 2 - Seattle, WA, USA
Duration: 12 May 1980 → 14 May 1980