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.
由于復(fù)合材料的材料性能分散性大，結(jié)構(gòu)所承受的載荷也具有不確定性，因此在設(shè)計中需要考慮復(fù)合材料層合結(jié)構(gòu)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層合板沖擊正面在壓縮載荷作用下為纖維基體剪切斷裂失效，沖擊背面則以分層損傷為主。
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-里茲法用來計算包含單一脫層的對稱正交鋪設(shè)層板在雙軸載荷作用下脫層屈曲的臨界載荷。