[1] Leissa A W. A review of laminated composite plate buckling [J]. Appl Mech Rev, 1987,40(5): 575～591.
[2] Chia C Y. Nonlinear Analysis of Plates [M]. New York: McGraw-Hill Inc, 1980
[3] Jensen D W, Lagace P A. Influence of mechanical coupling on the buckling and postbuckling of anisotropic plates [J]. AIAA J, 1988, 26(10): 1269～1277
[4] Zhang Y, Matthews F L. Initial buckling of curved panels of generally layered composite materials [J]. Composite Materials, 1983, 1(1): 3～30
[5] Zhang Y, Matthews F L. Postbuclding behavior of curved panels of generally layered composite materials [J]. Composite Materials, 1983, 1(2): 115～136
[6] Zhang Y, Matthews F L. Large deflection behavior of simply supported laminated panelsunder in-plane loading [J]. ASME J of Appl Mech, 1985, 52(3): 553～558
[7] Dong W L, Huang X Q. A Study of the postbuckling path of cylindrically curved panels oflaminated composite materials during loading and unloading [J]. ICCM-Ⅶ, 1989, 3; ApplMath and Mech (English Edition), 1990, 11(7): 651～657
[8] Underwood P. Dynamic relaxation [A]. In: eds T Belytschko & T J R Hughos. Computational Method for Transient Analysis [M]. Amsterdam: North-Holland, 1983
[9] Huang X Q. Application of the dynamic relaxahon method to the non-linear bending of composite laminates, ACTA Materiae Compositae Sinica, 1985, 2 (2): 47～51 (in Chinese)
[10] Huang X Q, Dong W L. Effects of transverse shear on the nonlinear bending of rectangular plates laminated of bimodular composite materials [J]. Appl Math and Mech (English Edition), 1987,8(1): 81～88
[11] Cassell A C, Hobbs R E. Numerical stability of dynamic relaxation analysis of nonlinear structures [J]. Int J Num Meth Engng, 1976, 10(6): 1407～1410.