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Composite Structures - v. 52, n. 1 (avril 2001)

Publié:	avril 2001

Articles dans ce numéro

Auteur(s)	Titre	Page(s)
Becker, Wilfried / Peng Jin, Pei / Lindemann, Jan	The "free-corner effect" in thermally loaded laminates	97-102
Ghiringhelli, Gian Luca / Masarati, Pierangelo / Mantegazza, Paolo	Analysis of an actively twisted rotor by multibody global modeling	113-122
Antona, Ettore / Frulla, Giacomo	Cicala's asymptotic approach to the linear shell theory	13-26
Ching Quek, Shu / Waas, Anthony M. / Hoffman, Jennifer / Agaram, Venkatesh	The crushing response of braided and CSM glass reinforced composite tubes	103-112
Williams, Todd O.	Efficiency and accuracy considerations in a unified plate theory with delamination	27-40
Ossadzow, Claire / Touratier, Maurice	An improved shear-membrane theory for multilayered shells	85-95
Di Sciuva, M. / Icardi, U.	Numerical assessment of the core deformability effect on the behavior of sandwich beams	41-53
Song, Ohseop / Librescu, Liviu / Jeong, Nam-Hui	Static response of thin-walled composite I-beams loaded at their free-end cross-section: analytical solution	55-65
Cheng, Zhen-Qiang / Batra, R. C.	Thermal effects on laminated composite shells containing interfacial imperfections	3-11
Icardi, U.	A three-dimensional zig-zag theory for analysis of thick laminated beams	123-135
Tessler, A. / Annett, M. S. / Gendron, G.	A {1,2}-order plate theory accounting for three-dimensional thermoelastic deformations in thick composite and sandwich laminates	67-84

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IssueID
38205
Publié(e) le:
25.10.2020
Modifié(e) le:
25.10.2020

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