Applied Mathematics and Mechanics (English Edition) ›› 1988, Vol. 9 ›› Issue (5): 441-448.

• 论文 • 上一篇    下一篇

NUMERICAL ANALYSIS OF EDGE EFFECT IN LAMINATED COMPOSITE STRUCTURES

叶碧泉, 周焕文   

  1. Wuhan University, Wuhan
  • 收稿日期:1986-11-05 出版日期:1988-05-18 发布日期:1988-05-18
  • 基金资助:

    Project Supported by the Science Fund of the Chinese Academy of Science

NUMERICAL ANALYSIS OF EDGE EFFECT IN LAMINATED COMPOSITE STRUCTURES

Ye Bi-quan, Chou Huan-wen   

  1. Wuhan University, Wuhan
  • Received:1986-11-05 Online:1988-05-18 Published:1988-05-18
  • Supported by:

    Project Supported by the Science Fund of the Chinese Academy of Science

摘要: In order to further study free edge effect in composite laminates, a new method is developed. This method is based on the perturbation and modified method of least square. In this paper, we emphatically discuss the solution within the boundary layer region, the so-called inner solution. As an example, we will discuss structures composed of two and four symmetric laminates.

关键词: satellite formation flying, relative motion, C-W’s equation, relative orbital element method, periodic solution

Abstract: In order to further study free edge effect in composite laminates, a new method is developed. This method is based on the perturbation and modified method of least square. In this paper, we emphatically discuss the solution within the boundary layer region, the so-called inner solution. As an example, we will discuss structures composed of two and four symmetric laminates.

Key words: satellite formation flying, relative motion, C-W’s equation, relative orbital element method, periodic solution

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