## ANSYS滑翔弹翼复合材料强度分析

Title  Strength analysis of composite wing glider
Abstract
As technology increasingly update, we consider not only limited aspects of the structure of the missile wing, but concerned about in terms of its materials, the rise of composite materials for the development of gliding brings more possibilities. Composite materials are light weight, stiffness and strength characteristics, as well as high fatigue strength, high shock resistance characteristics. Composite wing is the future direction of the glider research, we must first carry out the strength of the composite material wing stiffness analysis, in order to carry out further research. In this paper, ANSYS software for composite wing finite element mesh partition and using composites symmetrical layer and the plate, carbon fiber wing glider under static conditions, for four kinds of composite ply comparative study ways to give stress and deformation of the different contours of each wing of the overlay mode, comparative study wing stiffness and strength. 源自\$六l维,论:文w网)加7位QQ3249^114 www.lwfree.cn
Keywords  Missile wing; Finite element; Compound material; Strength;

1  引言    1
1.1  课题背景及意义    1
1.2  研究概况    1
1.2.1  复合材料概况    1
1.2.2  国内研究现状    2
1.2.3  国外研究现状    3
1.3  碳纤维复合材料的结构与性能    3
1.3.1  碳纤维的力学性能    3
1.3.2  碳纤维的物理性能    3
1.4  本文主要工作    4
2  碳纤维复合材料滑翔弹翼模型的建立    5
2.1  引言    5
2.2  力学的基本概念    5
2.2.1  平衡方程    5
2.2.2  应力    5
2.2.3  应变    6
2.2.4  抗拉强度    6
2.2.5  泊松比    6
2.3  偏微分方程    6
2.3.1  弹性体中任意一点的各分量    6
2.3.2  各向同性弹性力学基本方程    7
2.3.3  各向异性弹性力学的基本方程    9
2.4  本章小结    10
3  复合材料设计的基本理论与ANSYS有限元方法    11
3.1  有限元分析的基本概念    11
3.2  复合材料的组成    11
3.3  复合材料的设计理论    12
3.4  复合材料ANSYS有限元方法    12
3.5  本章小结    14
4  求解复合材料弹翼模型    15 源自\$六l维,论:文w网)加7位QQ3249^114 www.lwfree.cn