TY - JOUR
T1 - OPTIMIZATION METHOD FOR THE DETERMINATION OF THE IMPORTANT FLUTTER MODES.
AU - Nissim, Eliahu
AU - Lottati, I.
N1 - Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 1980
Y1 - 1980
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=0019151232&partnerID=8YFLogxK
U2 - 10.2514/6.1980-790
DO - 10.2514/6.1980-790
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AN - SCOPUS:0019151232
SN - 0273-4508
SP - 741
EP - 747
JO - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
JF - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
T2 - Collect Tech Pap AIAA ASME ASCE AHS Struct Struct Dyn Mater Conf 21st, Pt 2
Y2 - 12 May 1980 through 14 May 1980
ER -