@inproceedings{1b67e7d26cc045229741b1b503ef2b47,
title = "Optimum lay-ups for buckling of cylindrically curved laminated panels",
abstract = "A simple formula is proposed to calculate the critical buckling load of cylindrically curved composite panels (shallow shells) subjected to external uniform pressure. The buckling load is maximized with respect to the fiber orientation angles in all layers of the symmetrically laminated panel simply supported along the edges. The optimization is processed by following the layerwise optimization (LO) scheme In numerical examples, the optimum layups are obtained both by using the present formula and a general-purpose finite element (FEM) software, and the maximum buckling loads obtained by using the two methods are compared. The accuracy of the formula is discussed by the compassion. The optimum layups are obtained also by FEM and LO scheme for other boundary conditions.",
keywords = "Buckling load, Cylindrical panel, Laminated composite, LO method, Optimization, Shallow shell",
author = "Ryohei Sasaki and Shin, \{Eui Sup\} and Katsuhiko Sasaki and Yoshihiro Narita",
year = "2008",
language = "English",
isbn = "9784901381321",
series = "Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008",
pages = "319--322",
booktitle = "Progress of Composites 2008 in Asia and Australasia - Proceedings of the 6th Asian-Australasian Conference on Composite Materials, ACCM 2008",
note = "6th Asian-Australasian Conference on Composite Materials: Progress of Composites 2008 in Asia and Australasia, ACCM 2008 ; Conference date: 23-09-2008 Through 26-09-2008",
}