1) cross_ply laminate
正交叠层
1.
On the basis of the shear_lag theory,this paper studies the microstress redistributions induced by the interaction of failure of 90° layers and the breakage of some fibers in 0° layer in cross_ply laminates under tension in 0° direction.
基于剪滞理论，研究了在０°方向承受拉伸的复合材料正交叠层板由９０°层的破坏及０°层中部分纤维断裂相互作用所导致的细观应力重新分布。
2) cross-ply laminate
正交叠层板
1.
The transverse initial cracking of the cross-ply laminates in 90° ply by the action of the tensile loads in 0° ply direction was studied by establishing a layering shear-lag model conjunct with the linear elastic fracture mechanics.
建立一种分层剪滞模型 ,并结合线弹性断裂力学 ,研究了正交叠层板在受到沿 0°层方向的拉伸荷载作用下 ,90°层中产生横向基体开裂的破坏问题 。
2.
The transverse initial-failure in cross-ply laminates loaded in 0 degree fiber direction is first studied using the shear-lag model of finite sub-layers and incorporating the linear elastic fracture mechanics.
采用有限子层剪滞模型,并结合线弹性断裂力学,首先研究了正交叠层板在受到沿0o层方向的拉伸荷载作用下,90o层中产生横向初始开裂问题。
3) notched cross-ply laminate
割口正交叠层板
1.
Based on the shear-lag theory, a layering shear-lag model taking into account the interfacial damage was proposed and the stress redistributions for notched cross-ply laminates under tension were analyzed, from which both the length of the interfacial damage area and stress concentration factors in intact fibers at root of the notch were obtained.
在此基础上,采用细观统计破坏理论,研究了割口正交叠层板的拉伸破坏机理和强度,定量获得了残余拉伸强度与界面剪切强度的关系,所得结果与现有实验吻合较好。
2.
The stress redistributions for notched cross-ply laminates under tension were analyzed by establishing a layering shear-lag model, from which the stress concentration factors in intact fibers at the root of the notch were obtained.
在此基础上,采用复合材料的细观统计破坏理论,研究了割口正交叠层板的拉伸破坏强度,得到与现有实验较吻合的结果。
4) cross-ply(hybrid) laminate
正交(混杂)叠层
5) crossply laminate
正交叠层复合材料
6) Laminated orthotropic composite plate
正交各向异性叠层极
补充资料：层岩叠壑图
中国画。清代髡残作。纸本立轴。浅设色。画面景物繁复。上方左角大江浩淼，帆影依稀；右角山峰高峻，瀑流奔壑，山径左曲，至中幅复右折。近景绿树掩映，茅屋临溪。笔法苍秀醇厚，有雄奇磊落之致。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条