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

• Articles • Previous Articles     Next Articles

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

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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