建立了一个橡胶复合材料结构有限元分析模型。
A finite element model for rubber matrix composite structures is developed in this paper.
本文的另一个侧重面是复合材料结构动力学分析。
The other important aspect is the analysis of the structure dynamics of composite materials.
特别地，锁相热成像更适合用来检测复合材料结构。
In particular, Lock - in thermography is more suitable to detect composite material structure.
并给出典型复合材料结构元件的固化变形预测规律。
Also prediction results of cure induced deformation for composite structural elements are given.
研究了高模量碳纤维复合材料结构的电磁铆接工艺。
We have to find out how to do EMR successfully without causing damage in high modulus carbon fiber composites structure.
复合材料结构在小型无人驾驶飞机中占据着主导地位。
The composite already becomes the main material of UAV (unmanned aerial vehicle) structures.
复合材料的界面是影响复合材料结构与性能的关键因素。
The interfacial action plays an important effect to the structure and property of the composite materials.
所得结果可以为预测复合材料结构的声疲劳寿命提供参考。
The results can provide references for forecasting acoustic fatigue life of composite structures.
本文简要介绍了复合材料结构的数值计算模型的建立方法。
This paper presented several methods for establishing the model of composite structure by numerical method.
本文提出复合材料结构优化设计的一种新的多级优化设计方法。
Here presented a new multilevel optimization procedure for minimum weight design of composite structure.
试验表明，该系统可用于复合材料结构和蜂窝夹层结构的无损检测。
It is concluded that the system can be used in nondestructive detection of composite material and honeycomb structure.
论述了基于冲击威胁概念的复合材料结构冲击损伤容限可靠性分析方法。
An impact damage tolerance reliability analysis method was discussed for composite structures by introducing an impact threat concept.
为获得一种实时判别复合材料结构损伤的方法研究了属性测度及其识别。
This paper considered the attribute measurement and attribute measurement recognition to obtain a real-time damage-detecting method for composite materials and structure.
研究了钢-碳纤维组成的混合体系对水泥基复合材料结构和性能的影响。
The influences of hybrid fibre systems consisting of steel fibres and carbon fibres on the structural and properties of cementitious composites were studied.
本文探讨复合材料结构在设计、制造和应用过程中有关的一系列力学问题。
In this paper, a series of mechanical problems of structures for composite materials related to the design, manufacture and application are discussed.
根据此方法及虚拟仪器技术，设计开发了相应的复合材料结构损伤监测系统。
According to such method and the virtual instrument technique, an active damage monitoring system for composites is developed.
本文主要进行了一致性评判技术在直升机复合材料结构试验与分析中的应用研究。
This paper concentrates on the application research of consistency evaluation technique for the structural test and analysis used in composite material of helicopter.
本文以冲击实验和有限元分析研究了韧-脆复合材料结构中脆性材料的破碎问题。
The impact tests and the finite element method are used to investigate the fragmentation of brittle material in a composite structure consisting of PMMA and glass plates.
本文采用基于宏观和细观应力场两种不同方法来进行复合材料结构的损伤和破坏分析。
Based on both macro - and micro - stress fields, composite structures 'damage and failure are analyzed in this paper.
碳纤维复合材料管子是复合材料结构的基本元件，扭转变形是结构常见的基本变形形式。
Pipe of carbon composites is one of the basic components in composites structure, and torque deformation is one of the basic forms of the structure.
可设计性是复合材料的另一个特点，因此复合材料结构的优化设计也是研究的热点之一。
Designability is another feature of composites, which makes it possible to optimize a composite structure.
研究了利用形状记忆合金和液芯光纤对复合材料结构中的损伤进行自诊断、自修复的方法。
The method of self diagnosis and self repair for composite structure using shape memory alloy and adhesive liquid core optical fibers was studied.
《飞机复合材料结构修理》是飞行器制造工程(飞机维修方向)专业的一门专业技术课程。
Repair of aircraft Composite Structures is a new basic course of aircraft manufacturing engineering, aircraft maintenance directioned.
复合材料结构和复合材料加固结构的缺陷一般都是内部缺陷，传统的人工目测法很难检测。
As defects on composite material structure and composite material reinforced structure are inside, traditional testing method is hardly possible.
针对复合材料结构中广泛存在的固化变形现象，分析并讨论了其产生原因和可能的解决措施。
For phenomenon of cure induced deformation which is widely existed in composite structures, its cause and possible solution are discussed in this paper.
以剩余强度衰减理论为基础，建立了一种复合材料结构疲劳寿命可靠性定量分析的工程方法。
A analysis method of fatigue life reliability for composite structures is developed based on residual strength degradation theory.
对先进复合材料结构进行连续的实时在线监测是未来飞行器结构完整性研究的关键问题之一。
One of the critical tasks in the research of structural integrity for future's aircraft is to continuously on-line monitor the advanced composite structure in (near) real-time.
设计变量可包含复合材料结构的铺层方向角。广义气动力导数计及正交振动形态导数的影响。
The design variables include the ply orientations of composite material, and the derivatives of generalized aerodynamic forces involve normal modes derivatives.
在设计复合材料结构时，可以在基材的负载基础上，根据叠加法则推算出复合膜的破坏载荷。
Composite films fracture load can be calculated with plus theorem based on the load of base material when design the structure of the composite material.
在设计复合材料结构时，可以在基材的负载基础上，根据叠加法则推算出复合膜的破坏载荷。
Composite films fracture load can be calculated with plus theorem based on the load of base material when design the structure of the composite material.
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