Postbuckling behaviour of square compression loaded graphite epoxy panels with square and elliptical cut-outs

Thin-Walled Structures

Volumn 28, Issue 3-4, 1997, Pages 373-397

  Bailey, R ^a   Wood, J ^b  

^a GLASGOW CALEDONIAN UNIVERSITY   (United Kingdom)

^b UNIVERSITY OF THE WEST OF SCOTLAND   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPRESSIVE STRENGTH; COMPUTER SIMULATION; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; GRAPHITE FIBER REINFORCED PLASTICS; STRUCTURAL LOADS;

SOFTWARE PACKAGE ANSYS;

STRUCTURAL PANELS;

EID: 0031176127     PISSN: 02638231     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0263-8231(97)00052-9     Document Type: Article

References (30)

1. Levey, S., Wooley, R. M. and Kroll, W. D., Instability of a simply supported square plate with a reinforced circular hole in edge compression. Journal Research National Bureau of Standards, 1947, 39, 571-577.
2. Kumai, T., Elastic stability of the square plate with a central circular hole under edge thrust, Proceedings of the first Japan National Congress for Applied Mechanics, Japan, 1951, pp. 81-86.
3. Schlack, J. L., Elastic stability of pierced square plates. Exp. Mech., 1964, 4, 167-172.
4. Schlack, J. L., Experimental critical loads for perforated square plates. Proceedings of the Society of Experimental Stress Analysis, 1968, 25(1), 69-74.
5. Yoshiki, M., Fujita, Y., Kawamura, A. and Arai, H., Instability of plates with holes (first report). Proceedings of the Society of Naval Architects of Japan, December 1967, pp. 137-145.
6. Kawai, T. and Ohtsubo, H., A method of solution for the complicated buckling problems of elastic plates with combined use of Rayleigh-Ritz's procedure in the finite element method. Proceedings of the Second Conference of Matrix Methods in Structural Mechanics, Report AFFDL-TR-68-150, 1968, pp. 967-994.
7. Ritchie, D. and Rhodes, J., Buckling and post-buckling behaviour of plates with holes. Aeronautical Quarterly, 1975, XXIV, 281-296.
8. Nemeth, M. P., Buckling and postbuckling behaviour of compression loaded isotropic plates with cutouts. NASA TP-3024, September 1990.
9. Martin, J., Buckling and postbuckling of laminated composite square plates with reinforced central circular holes. Ph.D. Thesis, Case Western Reserve University, 1972.
10. Marshall, I. H., Little, W. and El Tayeby, M. M., The stability of composite panels with holes. Reinforced Plastics Congress, Brighton, UK, November 1984.
11. Marshall, I. H., Little, W., El Tayeby, M. M. and Williams, J., Buckling of perforated composite plates - An approximate solution. Proceedings of the Institution of Mechanical Engineers, C30/86, 1986.
12. Marshall, I. H., Little, W. and El Tayeby, M. M., Stability of composite panels with holes. In Mechanical Characterisation of Load Bearing Fibre Composite Laminates, chapter 17, eds. A. H. Cardon and G. Verchery. Elsevier Applied Science, Amsterdam, 1985.
13. Marshall, I. H., Little, W. and El Tayeby, M. M., Composite panels with circular cutouts: Some design guidelines. Proceedings of Reinforced Plastics Congress, Nottingham, UK, 1986, pp. 91-94.
14. Marshall, I. H., Little, W. and El Tayeby, M. M., Membrane stress distributions in post-buckled composite plates with circular holes. VI International Conference on Composite Materials ICCM & ECCM, Vol. 5, 1987, pp. 5.57-5.67.
15. Nemeth, M. P., Buckling behaviour of orthotropic composite plates with centrally located cutouts. Ph.D. Thesis, Virginia Polytechnic Institute and State University, VA, USA, May 1983.
16. Nemeth, M. P., Stein, M. and Johnstone, E. R., An approximate buckling analysis for rectangular orthotropic composite plates with centrally located cutouts. NASA Tp 2528, February 1986.
17. Nemeth, M. P., A buckling analysis for rectangular orthotropic plates with centrally located cutouts. NASA TM 86263, December 1984.
18. Nemeth, M. P., Buckling behaviour of compression-loaded symmetrically laminated angle-ply plates with holes. AIAA Journal, 1988, 26(3), 330-336.
19. Kantorovich, L. and Krylov, V. I., Approximate Methods of Higher Analysis. Interscience, 1964.
20. Vandenbrik, J. and Kamat, P., Post-buckling response of isotropic and laminated composite square plates with circular holes. Proceedings of the International Conference of Composite Materials, San Diego, California, 1985, 1393-1409.
21. Larsson, P. -L., On the buckling of orthotropic compressed plates with circular holes. Composite Structures, 1987, 7, 103-121.
22. Buskell, N., Davies, G. A. O. and Stevens, K. A., Postbuckling failure of composite panels. Composite Structures, 1985, 3, 677-691.
23. Yasui, Y. and TsuKamura, K., Buckling strength of rectangular FRP with a hole. Journal of the Society of Material Science (Japan), 1988, 37, 1050-1056.
24. Horn, W. J. & Rouhi, M., A comparison of the post-buckling behaviour of metallic and composite plates with centrally located cutouts. National Institute for Aviation Research Report No. 89-11, The Wichita State University, July 1989.
25. Rouhi, M. and Horn, W. J., A comparison of the Post-buckling behaviour of metallic and composite plates with centrally located cutouts. National Institute for Aviation Research Report No. 90-14, The Wichita State University, May 1990.
26. Nemeth, M. P., Buckling and post-buckling behaviour of square compression-loaded graphite-epoxy plates with circular cutouts. NASA TP-3007, August 1990.
27. Yasui, Y., The buckling of rectangular composite plates with cutout under uniaxial and biaxial compression. Eighth International Conference on Composite Materials, eds. S. W. Tsai and G. S. Springer. Honolulu, HI, USA, July 1991.
28. ANSYS User's Manual for Revision 5.0. Vol. IV, Theory, February 1994.
29. Zienkiewicz, O. C., The Finite Element Method. McGraw-Hill, London, 1977.
30. Bathe, K. J., Finite Element Procedures in Engineering Analysis. Prentice-Hall, Englewood Cliffs, NJ, 1982.