TECHNICAL PAPERS
Oct 1, 2005

Buckling of Laminated Composite Rectangular Plates

Publication: Journal of Aerospace Engineering
Volume 18, Issue 4

Abstract

The present study estimates the critical/buckling loads of laminated composite rectangular plates under in-plane uniaxial and biaxial loadings. The formulation is based on the first-order shear deformation theory and von-Karman-type nonlinearity. Chebyshev series is used for spatial discretisation and quadratic extrapolation is used for linearization. An incremental iterative approach is used for estimation of the critical load. Different combinations of simply supported, clamped and free boundary conditions are considered. The effects of plate aspect ratio, lamination scheme, number of layers and material properties on the critical loads are studied.

Get full access to this article

View all available purchase options and get full access to this article.

References

Adali, S., Aricher, A., and Verijenko, V. E. (1997). “Optimization of shear deformable laminated plates under buckling and strength criteria.” Compos. Struct., 39(3/4), 167–178.
Chattopadhyay, A., and Radu, A. G. (2000). “Dynamic stability of composite laminates using higher-order theory.” Comput. Struct., 77, 453–460.
Fox, L., and Parker, I. B. (1968). Chebyshev polynomials in numerical analysis, Oxford University Press, London.
Gu, H., and Chattopadhyay, A. (2000). “Three-dimensional elasticity solution for buckling of composite laminates.” Compos. Struct., 50, 29–35.
Hause, T., Johnson, T. F., and Librescu, L. (2000). “Effect of face sheet anisotropy on buckling and post buckling of flat sandwich panels.” J. Spacecr. Rockets, 37(3), 331–341.
Hwang, S., and Liu, G. (2001). “Buckling behaviour of laminates with multiple delaminations under uniaxial compression.” Compos. Struct., 53, 235–243.
Khdeir, A. A., and Librescu, L. (1988). “Analysis of symmetric cross ply laminated elastic plates using higher order theory: Part II—Buckling and free vibration.” Compos. Struct., 9, 259–277.
Kim, K. D. (1996). “Buckling behaviour of composite panels using the finite element method.” Compos. Struct., 36, 33–43.
Matsunaga, H. (2000). “Vibration and stability of cross-ply laminated composite plates according to a global higher-order plate theory.” Compos. Struct., 48, 231–244.
Moita, J. S., Mota Soares, C. M., and Mota Soares, C. A. (1999). “Buckling and dynamic behaviour of laminated composite structures using a discrete higher-order displacement model.” Comput. Struct., 73, 407–423.
Nair, S. L., Singh, G., and Rao, G. V. (1996). “Stability of laminated composite plates subjected to various types of in-plane loadings.” Int. J. Mech. Sci., 38(2), 191–202.
Narita, Y., and Leissa, A. (1990). “Buckling studies for simply supported symmetrically laminated rectangular plates.” Int. J. Mech. Sci., 32(11), 909–924.
Noor, A. K. (1975). “Stability of multilayered composite plates.” Fibre Sci. Technol., 8, 81–89.
Owen, D. R. J., and Li, Z. H. (1987). “A refined analysis of laminated plates by finite element displacement methods—II: Vibration and stability.” Comput. Struct., 26(6), 915–923.
Shukla, K. K., and Nath, Y. (2000). “Nonlinear analysis of moderately thick laminated rectangular plates.” J. Eng. Mech., 126(8), 831–838.
Sundarsen, P., Singh, G., and Rao, G. V. (1996). “Buckling and postbuckling of moderately thick laminated rectangular plates.” Comput. Struct., 61(1), 79–86.
Turvey, G. J., and Marshall, I. H. (1995). Buckling and postbuckling of composite plates, Chapman and Hall, London.
Wang, W. J., Tseng, Y. P., and Lin, K. J. (1996). “Stability of laminated plates using finite strip method based on a higher-order theory.” Compos. Struct., 34, 65–76.
Zhang, J., Li, Q., and Shu, Y. (2000). “Nonlinear stability of unsymmetrically laminated angle-ply shear-deformable plates in bi-axial compression.” Thin-Walled Struct., 38, 1–6.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 18Issue 4October 2005
Pages: 215 - 223

History

Received: Oct 30, 2003
Accepted: Oct 15, 2004
Published online: Oct 1, 2005
Published in print: Oct 2005

Permissions

Request permissions for this article.

Authors

Affiliations

K. K. Shukla [email protected]
Reader, Applied Mechanics Dept., M.N.N.I.T., Allahabad-04, India. E-mail: [email protected]
Professor, Applied Mechanics Dept., Indian Institute of Technology, Delhi-16, India. E-mail: [email protected]
E. Kreuzer
Professor, TUHH, Meerestechnik II, Essendorfer Str. 42, 21073 Hamburg, Germany.
K. V. Kumar
Graduate Student, Applied Mechanics Dept. Indian Institute of Technology, Delhi-16, India.

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share