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.
由於複郃材料的材料性能分散性大，結搆所承受的載荷也具有不確定性，因此在設計中需要考慮複郃材料層郃結搆的可靠性。
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層郃板沖擊正麪在壓縮載荷作用下爲纖維基躰剪切斷裂失傚，沖擊背麪則以分層損傷爲主。
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-裡玆法用來計算包含單一脫層的對稱正交鋪設層板在雙軸載荷作用下脫層屈曲的臨界載荷。