A model is proposed for predicting the effective longitudinal shear modulus of fiber reinforced composite materials.
本文给出一个计算单向纤维增强复合材料纵向剪切模量的模型。
In the paper the elastoplastic constitutive relations of unidirectional fiber reinforced composite materials were modeled numerically.
本文对单向连续纤维增强复合材料的弹塑性本构关系进行了数值模拟。
The friction and wear tests of the self lubricating bearing made of carbon fiber reinforced copper matrix composite materials are arranged by uniform design that can greatly reduce the test duration.
根据均匀设计原理，对碳纤维增强铜基复合材料的磨损试验参数予以科学排列，不仅减少了试验次数，而且提高了试验数据统计结果的可靠性。
Interface characteristics of carbon fiber reinforced copper matrix composite materials with various interface states and their effect on the flexural strength of the composites had been studied.
研究了三种不同界面结合状态(机械结合、溶解结合、反应结合)的碳纤维增强铜复合材料的界面结构及其对复合材料弯曲强度的影响。
The equivalence heat conduction coefficients of fiber reinforced and hollow sphere filled composite materials would be particularly proposed.
具体地导出了单向纡维复合材料和空心微珠复合材料等效导热系数的组分设计公式。
With practical examples, I have calculated the unidirectional fiber-reinforced composite material engineering constants and discussed the finite element issue of anisotropic materials.
结合工程实例，计算了单向纤维增强复合材料工程常数，探讨了各向异性材料的有限元问题。
The present invention is one kind of composite materials of fiber reinforced sulfaluinous cement with high water permeability.
本发明是特别适用于油田的一种纤维增强硫铝酸盐高渗透水泥石复合材料。
A diamond coated drill capable of drilling holes in fiber reinforced composite materials.
一种能够在纤维增强复合材料中钻孔的金刚石涂敷的钻头。
Carbon fiber reinforced plastic (CFRP) is an important kind of composite materials to produce light aircraft or large model aircraft.
碳纤维增强树脂基复合材料是生产轻型飞机或大型航模的重要材料。
XU H J. Metal matrix composite and ceramic matrix composite reinforced by SiC fiber[J]. Aerospace Materials & Technology, 1994, (6):13-18.
[20] 徐海江。碳化硅纤维增强的金属基和陶瓷基复合材料[J]。宇航材料工艺，1994，（6）：13-18。
XU H J. Metal matrix composite and ceramic matrix composite reinforced by SiC fiber[J]. Aerospace Materials & Technology, 1994, (6):13-18.
[20] 徐海江。碳化硅纤维增强的金属基和陶瓷基复合材料[J]。宇航材料工艺，1994，（6）：13-18。
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