航空学报 > 1990, Vol. 11 Issue (11): 556-560

复合材料层板结构在冲击载荷作用下非线性动力分析

素瑞芬1, 胡茂和1, 孙淑苓1, 沈成武2   

  1. 1. 直升机设计研究所 ;2. 武汉大学
  • 收稿日期:1989-10-25 修回日期:1990-05-18 出版日期:1990-11-25 发布日期:1990-11-25

NONLINEAR DYNAMIC ANALYSIS OF LAMINATED COMPOSITE STRUCTURE UNDER IMPACT LOADS

Qin Ruifen1, Hu Maohe1, Sun Shulin1, Shen Chengwu2   

  1. 1. Chinese Helicopter Research and Development Institute;2. Wuhan University
  • Received:1989-10-25 Revised:1990-05-18 Online:1990-11-25 Published:1990-11-25

摘要: <正> 复合材料结构非线性动力分析具有一定难度,本文在这方面作了些探索,以期为复合材料结构在冲击载荷作用下非线性动力分析提供一种途径。本文方法所编制的计算程序计算两个算例。第二个算例,是某飞机水平尾翼在特殊飞行中,承受瞬态冲击分布外压载荷,其作用时间只有几毫秒。用此法计算得到的响应与试验结果比较吻合。

关键词: 冲击载荷, 变动的拉格朗日方法, 增量, 层板结构

Abstract: Hill's plastic theory of anisotropic materials is used and nonlinear finite element equations of laminated plate structure by Updated Lagrange method is set up in this paper. These dynamic equations are solved by incremental and Wilson-θ method. Furthermore, using a special technique to deal with pressure-boundary conditions, it also considers transverse shear and material extension-compression moduli. Finally, the local failure of strength of anisotropic materials is discussed.

Key words: impact-load, Updated-Langrange method, incremental, laminated plate structure.