Buckling of laminated composite stiffened panels subjected to in-plane shear: A parametric study-Reference-Cited by-同舟云学术

Buckling of laminated composite stiffened panels subjected to in-plane shear: A parametric study

Published:2006-03 Issue:3 Volume:44 Page:354-361
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Mallela Upendra K.,Upadhyay Akhil

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference19 articles.

1. Stroud WJ, Agranoff N. Minimum-mass design of filamentary composite panels under combined loads: design procedure based on simplified equations. TN D-8257, NASA; 1976.

2. A review of laminated composite plate buckling;Leissa;ASME Appl Mech Rev,1987

3. Mechanics of composite structural elements;Altenbach,2004

4. Load-carrying capacity of thin-walled composite structures;Kolakowski;Compos Struct,2005

5. Buckling behaviour of composite panels using the finite element method;Kim;Compos Struct,1996

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