4Timoshenko S, Woinowsky - Krieger S. Theory of plates and shells [M]. 2nd. New York: McGraw - Hill Book Company, 1959:364-370.
5徐芝纶.弹性力学(下册)[M].3版.北京:高等教育出版社,1992:172-176.
6Seide P. The effect of longitudinal stiffeners located on one side of a plane on the compressive buckling stress of the plate stiffener combination, NASA TN - 2873 [R]. Washington: NASA, 1953.
7Schmit L A, Mehrinfar M. Multilevel optimum design of structures with fiber- composite stiffened- panel components [J]. AIAA Journal, 1982, 20(1): 138-14:7.
8Navin Jaunky, Norman F Knight Jr, Damodar R Ambur. Optimal design of grid-stiffened composite panels using global and local buckling analyses [J]. AIAA Journal of Aircraft, 1998, 35(3): 478-486.
9Wodesenbet E, Kidane S, Pang Su - Seng. Optimization for buckling loads of grid stiffened composite panels[J]. Composite Structures, 2003, 60: 159-169.
10Chen Hongji, Tsai S W. Analysis and optimum design of composite grid structures[J].Journal of Composite Materials, 1996, 30(4): 503-533.
