composite laminate

基本解释

Due to the scattered properties of composite materials, the random variation of loads, the reliability of composite laminate structures must be considered in design process.
由于复合材料的材料性能分散性大，结构所承受的载荷也具有不确定性，因此在设计中需要考虑复合材料层合结构的可靠性。
However, the damage modes of the impact surface and the impact back surface for composite laminate 5224/G827 are shear fracture of fiber and substrate and delamination respectively.
而5224/G827层合板冲击正面在压缩载荷作用下为纤维基体剪切断裂失效，冲击背面则以分层损伤为主。
The Rayleigh-Ritz method is used to calculate the critical load at which delamination buckling will occur for a symmetric cross-ply composite laminate containing a single delamination.
瑞雷-里兹法用来计算包含单一脱层的对称正交铺设层板在双轴载荷作用下脱层屈曲的临界载荷。