准确预测含分层损伤层合板的剩余压缩强度，对复合材料具有十分重要的意义。
Predicting residual compression strength of composite laminates with delamination is a very important research subject for Engineering composite structure designers.
结果表明，试验件含分层损伤面积越大，其破坏载荷越大，而对应的破坏应变越大，因此分层损伤会降低复合材料层合板的承载力和刚度。
The results of experimentation indicate that the failure load of the delaminated composite panels declines and the failure strain increases as the increasing of delaminated area.
洪明，陈浩然，含分层损伤复合材料层合板声激励下振动特性研究，船舶力学，2004，8（2）， 94-100；
Hong Ming, Chen Haoran, Effect of Plane Wave Exciation on Vibration Behavior of Laminated Composite Plate with Delamination, Journal of Ship Mechanics, 2004, 8(2), 94-100.
洪明，陈浩然，含分层损伤复合材料层合板声激励下振动特性研究，船舶力学，2004，8（2）， 94-100；
Hong Ming, Chen Haoran, Effect of Plane Wave Exciation on Vibration Behavior of Laminated Composite Plate with Delamination, Journal of Ship Mechanics, 2004, 8(2), 94-100.
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