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contributor authorNarendra S. Khot
contributor authorJeffrey V. Zweber
date accessioned2017-05-08T21:16:07Z
date available2017-05-08T21:16:07Z
date copyrightJanuary 2003
date issued2003
identifier other%28asce%290893-1321%282003%2916%3A1%2819%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44974
description abstractThis paper is concerned with designing an optimum composite flexible wing structure to enhance flutter speed by imposing modal frequency distribution constraints and comparing it with an optimum design obtained with the flutter velocity constraint. The composite wing is subjected to three flight conditions to satisfy stress constraints in addition to modal frequency distribution or flutter constraints. The multidisciplinary optimization system
publisherAmerican Society of Civil Engineers
titleDesign of Flutter Characteristics of Composite Wings Using Frequency Constraint Optimization
typeJournal Paper
journal volume16
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2003)16:1(19)
treeJournal of Aerospace Engineering:;2003:;Volume ( 016 ):;issue: 001
contenttypeFulltext


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