composite laminate发音

意思翻译

复合层压板

复合材料层压板

相似词语短语

composite───v.合成（图片）；使混合；n.复合材料，合成物；综合提案；菊科植物；混合柱式；（嫌疑犯的）合成照片；adj.复合的，合成的；（火车车厢）综合的；（柱式）混合的；菊科的

laminate───adj.薄片状的；层状的；v.将锻压成薄片；分成薄片；n.薄片制品；层压制件

laminate countertops───层压台面

durion laminate───durion层压板

laminate flooring───强化地板；复合地板；层压木地板

formica laminate───formica层压板

recurved composite bow───[体]两端反曲合成材料弓

climatize laminate flooring───气候强化木地板

laminate wood flooring───强化木地板

双语使用场景

Parametric FEM technique is used to analyze the mechanical performance and structural reliability of composite laminate structures. The parametric FEM code based on ANSYS is given.───参数化有限元技术分析复合材料层合结构力学性能和结构可靠度的方法，并基于ANSYS软件平台开发相应的参数化有限元程序。

method was also used to measure strain in the tensile test of a composite laminate plate. The results agree fairly well with those obtained by the conventional measurement.───并进行了复合材料板拉伸试验，复合材料平板实验计算结果和应变电测法得到的结果进行了对比，实验表明两种测量方法得到的结果相吻合。

The change in critical load value of both composite laminate plates with embedded and through-width delamination shows the same pattern for various delamination size.───对不同的脱层损伤尺寸，层合板分别有整体、混合和局部三种屈曲模态，穿透脱层和埋藏脱层的层合板其临界载荷的变化规律是相同的。

Delamination is one of the important defect forms of composite laminate construction.───局部分层屈曲是复合材料层壳结构的一种重要损伤形式。

For instance the material forming the composite laminate may be reinforced, and the resin forming the impact indicator may be un-reinforced.───例如，制造复合层压制品的材料可以是加强的，而制造撞击指示物的树脂可以是非加强的。

The fracture mechanics feature of elliptical delaminations in a composite laminate is studied.───对复合材料层板中椭圆分层的断裂力学问题进行了研究。

The first and second scrim layers constitute exposed surfaces of the composite laminate.───上下两层薄亚麻仍作为复合材料片层的表层裸露在外。

The transient response of delaminated composite laminate under low velocity is discussed in the present paper.───研究了含脱层损伤的复合材料层板在低速冲击下的瞬态响应问题。

Study of Delamination Buckling for a Symmetric Cross-ply Composite Laminate under Uniaxial Loads───单轴载荷作用下对称正交铺设层合板的脱层屈曲研究

英语使用场景

In this paper, Full Strain Design method and Sublaminate are combined to optimize fibre - enhanced composite laminate.

The stacking sequence of composite laminate was calculated at given in - plane geometry and bend factors.

Based on two hypothesis, a new kind of four parameters model was posed that used on S N curve over long and middle life range of composite laminate.

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.

Finally aeroelastic tailoring technique of composite laminate is applied to forward - wing structure to improve divergence speed.

The effect of hole diameter on bearing capacity of alloy plate and composite laminate was analyzed.

The transient response of delaminated composite laminate under low velocity is discussed in the present paper.

The first and second scrim layers constitute exposed surfaces of the composite laminate.