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.

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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.

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Stress singularity and inhomogeneity in composite laminates . 6.

复合材料结构之应力奇异性相关问题.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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