Optimum buckling design of composite stiffened panels using ant colony algorithm
نویسندگان
چکیده
منابع مشابه
Optimum Buckling Design of Composite Stiffened Panels Using Ant Colony Algorithm
Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to uniform biaxial compressive load. In the optimization for the maximum buckling load without weight penalty, the panel skin and the stiffened laminate stacking sequence, thickne...
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Optimum Design of Composite Plates under Thermal Buckling Loads using Imperialist Competitive Algorithm
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Composite stiffened cylindrical shells are widely used as primary elements in aerospace structures. In the recent years, there has been a growing research interest in optimum design of composite stiffened cylindrical shell structures for stability under buckling load. This paper focuses upon the development of an efficient optimization of ring-stringer stiffened cylindrical shell. The opti...
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ژورنال
عنوان ژورنال: Composite Structures
سال: 2010
ISSN: 0263-8223
DOI: 10.1016/j.compstruct.2009.09.018