laminates

In composite laminates there are four basic failure modes: matrix cracking, delamination, fiber breakage and debonding.

复合材料层合板中存在四种基本的失效模式,即: 基体开裂 、 分层 、 纤维断裂及脱粘.

The three - dimensional exact solution methods for dynamic problems a finitely long piezoelectric composite laminates are studied.

有限长压电层合板结构动态问题的三维精确解研究.

Stress singularity and inhomogeneity in composite laminates . 6.

复合材料结构之应力奇异性相关问题.

By means of velocity feedback control agolrithm the active vibration control of laminates is fulfilled.

并采用速度反馈控制实现了层合板的主动振动控制.

Transverse cracking of matrix is a main damage type of cross - ply laminates.

基体横向开裂是复合材料正交层板的主要损伤类型.

The rehabilitation of reinforced concrete structures with CFRP laminates is a new reinforcement technique.

碳纤维布加固混凝土结构是一种新型的结构加固方法.

The direction stabilizer of aircraft can be improved by optimizing the composite laminates of vertical stabilizer.

通过优化垂尾复合材料蒙皮铺层体系,可以减少垂直尾翼的气动变形,进而改善飞机的方向安定性.

Decorative Laminates, Used Clothing, Rice, Sugar, Cement and Sand.

采购产品装饰积层塑料板,二手的衣服, 大米, 糖, 水泥和沙子.

The given solution satisfies all fundamental equations of elasticity and continuity conditions between the laminates.

此解满足层合板的基本方程和层间连续条件.

The behaviors and effective factors of laminates under flexural stress are analysed in this paper.

本文分析、讨论了积层板材料,在弯曲应力下的各种性能及影响因素.

These versatile laminates provide extremely high impact resistance and absorb total impact energy without spalling.

这些通用板材具有高抗冲击性,能吸收所有冲击能量而不碎裂.

A comprehensively coupled thermo - piezoelectric - mechanical model of composite laminates with single surface bonded piezoelectricapplied loads, is developed.

本文针对一种单面粘贴压电材料的复合材料层合板结构,建立了一种热 - 机-电完全耦合模型.

The failure analysis methods for composite laminates have been also discussed in this paper.

本文还讨论了复合材料中的失效分析方法.

The ideas and methods on the structure design of composite laminates are put forward.

从合层板的弯曲刚性出发,提出了复合材料层合板的结构设计的思想和方法.

The characteristics of interlayer metal have effect on the performance of whole laminates.

夹层金属材料本身的性能对叠层材料整体的性能也有一定的影响.