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对复合材料层合板做面板，蜂窝做夹芯的夹层结构在受到弯、扭载荷作用下的稳定性进行了研究。面板采用对称铺层、等高度蜂窝夹芯，利用能量法对临界载荷进行了计算并给出了一些计算曲线。
The sandwich structure made of honeycomb sandwich panels and composite honeycomb panels was studied under the bending and twisting loads. The panel adopts symmetrical lamination and isometric honeycomb sandwich. Using the energy method, the critical load is calculated and some calculation curves are given.