TECHNICAL PAPERS
Oct 15, 2003

Dynamic Stability of Laminated Composite Curved Panels with Cutouts

Publication: Journal of Engineering Mechanics
Volume 129, Issue 11

Abstract

The present investigation deals with the dynamic stability behavior of laminated composite curved panels with cutouts subjected to in-plane static and periodic compressive loads, analyzed using the finite element method. A generalized shear deformable Sanders’ theory with tracers is used in this study. Numerical results obtained for vibration and buckling of composite panels with cutouts compare well with literature. The principal dynamic instability region of composite perforated panels is obtained using Bolotin’s approach. The study reveals that curved panels with cutouts depict higher stiffness with the addition of curvatures. The laminated hyperbolic paraboloid panel shows the highest stiffness with the onset of instability at higher excitation frequencies. The effect of curvature in laminated composite curved panels is reduced with an increase in size of the cutout. The principal instability regions are influenced by the lamination parameters. Thus, the laminate construction, coupled with cutout geometry, can be used to the advantages of tailoring during design of composite structures for practical applications.

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Information & Authors

Information

Published In

Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 129Issue 11November 2003
Pages: 1245 - 1253

History

Received: Mar 12, 2002
Accepted: Apr 23, 2003
Published online: Oct 15, 2003
Published in print: Nov 2003

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Authors

Affiliations

S. K. Sahu
Assistant Professor, Dept. of Civil Engineering, National Institute of Technology, Rourkela, India.
P. K. Datta
Professor, Dept. of Aerospace Engineering, Indian Institute of Technology, Kharagpur, India.

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