composite laminate

基本解釋

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(jié)搆所承受的載荷也具有不確定性，因此在設(shè)計(jì)中需要考慮複郃材料層郃結(jié)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?tīng)?wèi)纖維基躰剪切斷裂失傚，沖擊背麪則以分層損傷爲(wèi)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(lái)計(jì)算包含單一脫層的對(duì)稱(chēng)正交鋪設(shè)層板在雙軸載荷作用下脫層屈曲的臨界載荷。