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Optimum design for buckling of plain and stiffened composite axisymmetric shell panels/shells

✍ Scribed by Biswajit Tripathy; K.P. Rao

Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
740 KB
Volume
25
Category
Article
ISSN
0263-8223

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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