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.
优化结果表明，从现代复合材料的应用与复合材料结构优化设计两方面入手进行汽车大型承载部件的轻量化研究，是非常有效的方法。
The optimized result proves it effective to do lightweight study on automobile's large-size load parts from the point of both the applicati…
提出一种面向设计的复合材料旋翼桨叶结构动力优化方法。
A design oriented method for the dynamic design optimization of composite rotor blades is presented.
通过结构优化设计可以获得重量轻刚度好的复合材料火炮身管。
Light weight and high stiffness composite material barrel can be obtained by a structure optimal design.
本文总结了复合材料旋翼浆叶结构动力优化设计的研究工作。
A research for structural dynamic optimization design of composite rotor blades is summarized.
论文以大展弦比飞翼布局机翼蒙皮的优化设计为背景，开展了复合材料层压板结构的优化设计工作。
In this paper, an effective design optimization method for High-aspect-ratio composite wing skin is presented.
建立复合材料的有效性质与微结构参数的关联，是复合材料优化设计的基础。
Correlating the effective properties of composite materials with their microstructures is a basis for optimization design of composite materials.
优化设计方法在复合材料结构设计中起着十分重要的作用。
The optimization design method is very useful in the structure design of composites.
它将复合材料翼面结构综合优化设计问题分解成两个易于求解的子问题：顶层优化设计和底层优化设计。
HDO divides the integrated optimization of composite wing structures into two sub-problems that are easy to be solved: upper level optimization and lower level optimization.
应用JIFEX软件对大型通信卫星主承力结构——中心承力筒的复合材料结构进行优化设计。
The optimal design of composite structures of principle bearing cylinder in large scale communication satellites is performed with JIFEX software.
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.
文中首先对复合材料结构进行了有限元分析，在此基础上提出对复合材料层合板的铺层角度、铺层厚度的优化设计算法。
After the structure is analyzed by FEM, an algorithm of ply orientation Angle optimization and ply thickness optimization is presented.
这种基于可靠性的结构优化设计可明显地提高复合材料结构的设计质量，使得复合材料结构既安全可靠又经济合理。
Such a structural optimum design based on the reliability can increase the design quantity and obtain obvious economic benefit, that is to say, the structure is both safe and economical.
提出一种面向设计的复合材料旋翼桨叶结构动力优化方法。
A new way to solve dynamical response of rotor blade in helicopter.
提出一种面向设计的复合材料旋翼桨叶结构动力优化方法。
A new way to solve dynamical response of rotor blade in helicopter.
应用推荐