Issue 50

O. Mouhat et alii, Frattura ed Integrità Strutturale, 50 (2019) 126-140; DOI: 10.3221/IGF-ESIS.50.12 140 DOI: 10.1007/s11709-014-0247-9. [6] Kachanov, L.M. (1988). Delamination Buckling of Composite Materials, Kluwer Academic Publishers, Dordrecht (The Netherlands). [7] Wright, J. E. (2006). Compound bifurcations in the buckling of a delaminated. Composite structure. Nonlinear Dynamic 43(1–2), pp. 59–72 . DOI: 10.1007/s11071-006-0751-0. [8] Short, G., Guild, F. J., Pavier, M. J. (2002). Delamination in flat and curved composite laminates subjected to compressive load. Composite Structure, 58(2), pp. 249–258. DOI: 10.1016/S0263-8223(02)00052-1. [9] Hunt, G. W., Butler, B., Almond, D. P., Wright, J. E. (2004). Nonlinear modeling of delaminated structures. AIAA J 42(11), pp. 2364–2372. DOI: 10.2514/1.5981. [10] Mallela, U. K., Upadhyay (2006). Buckling of laminated composite stiffened panels subjected to in-plane shear: a parametric study. Thin-Walled Structures, 44(3), pp. 354–361. DOI: 10.1016/j.tws.2006.03.008. [11] Kistler, L. S., Waas, A. M. (1998). Experiment and analysis on the response of curved laminated composite panels subjected to low velocity. Journal of Impact Engineering, 21(9), pp. 711–736. DOI:10.1016/S0734-743X(98)00026-8. [12] Singh, S. B., Kumar, D. (2008). Post-buckling response and failure of symmetric laminated plates with rectangular cutouts under uniaxial compression. Structural Engineering and Mechanics 29(2), pp. 455–467. DOI:10.12989/sem.1997.5.4.433. [13] Zhang, Y., Rheeb, K. Y., Parka, S.-J. (2017). Nanodiamond nanocluster-decorated grapheme oxide/epoxy Nano composites with enhanced mechanical behavior and thermal stability. Composites Part B: Engineering, 114, pp. 111- 120. DOI:10.1016/j.compositesb.2017.01.051. [14] Gal, E., Levy, R., Abramovich, H., Pavsner, P. Buckling analysis of composite panels. (2006). Composite structure, 73(2), pp.179–185. DOI : 10.1016/j.compstruct.2005.11.052. [15] Kim, Y. H., Noor, A. K. (1996). Buckling and post-buckling of composite panels with cutouts subjected to combined loads, Finite Elements in Analysis and Design, 22(2), pp. 163–185. DOI: 10.1016/0168-874X (95)00052-U. [16] Leissa, A.W. (1987). Review of laminated composite plate buckling. ASME Appl. Mech. Rev., 40 (5), pp. 575–591. DOI: 10.1115/1.3149534. [17] Broekel,J., Prusty,G. (2004).Experimental and theoretical investigations on stiffened and unstiffened composite panels under uniform transverse loading. Composite Structure, 63, pp. 293-304. DOI : 10.1016/S0263-8223(03)00178-8. [18] SudhirSastry, Y. B., Pattabhi, R., Madhavi, N., Krishna, Y. (2015). Buckling analysis of thin wall stiffened composite panels. Computational Materials Science. 96, pp. 459–471. DOI: 10.1016/j.commatsci.2014.06.007. [19] L. A. (1995). Finite elements for post-buckling analysis. II -Application to composite plate assemblies, Computer Structure, 56 (6), pp. 1019–1028. DOI:10.1016/0045-7949(94)00573-L. [20] Reddy, J. N. (1997). Mechanics of laminated composite plates. CRC Press. New York. [21] Riks, E. (1979). An incremental approach to the solution of snapping and buckling problems, International Journal Solids Structures, 15, pp. 524–551. DOI: 10.1016 /0020-7683(79)90081-7. [22] Zienkiewicz, O. C. and Taylor, R. L. (1991). The Finite Element Method.4 th Edn.McGraw-Hill, London.

RkJQdWJsaXNoZXIy MjM0NDE=