节点文献

力学在飞机结构设计中的应用与发展

APPLICATION AND DEVELOPMENT OF MECHANICS ON AIRCRAFT STRUCTURAL DESIGN

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 庄茁王向东张朝晖林勇文赵志明滕锦王璞

【Author】 ZHUANG Zhuo1 , WANG Xiang-dong2 , ZHANG Zhao-hui1 , LIN Yong-wen1 , ZHAO Zhi-ming1 , TENG Jin1 , WANG Pu1 (1. School of Aerospace, Tsinghua University, Beijing 100084, China; 2. College of Mechanical Engineering, Beihua University, Jilin 132021, China)

【机构】 清华大学航天航空学院北华大学机械工程学院清华大学航天航空学院 北京100084吉林132021北京100084

【摘要】 首先阐述了飞机结构中的力学问题。基于我们近几年的研究工作,从若干方面介绍了力学在飞机结构设计中的应用与发展,如机身的广布疲劳损伤蔓延的断裂力学计算和风险评估,鸟撞驾驶舱盖和起落架落震的强度问题,以及低速冲击作用下机翼的复合材料层合板的脱层和基体断裂问题等。

【Abstract】 The mechanical problem related to the aircraft structure design is described. Based on the research and development works in recent a few years, some applications and development for the mechanics used in the aircraft structure design are introduced, for example, fracture mechanics computation and risk evaluation for the widespread fatigue damage (WFD) in the fuselage, the strength problems for the windshield against the bird-impact and dynamic problems of the landing gear, as well as the delamination and matrix cracking in the composite laminates under the low-velocity impact.

  • 【文献出处】 工程力学 ,Engineering Mechanics , 编辑部邮箱 ,2007年S2期
  • 【分类号】V214
  • 【被引频次】9
  • 【下载频次】1052
节点文献中: 

本文链接的文献网络图示:

本文的引文网络