导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (11): 556-560.

• 论文 • Previous Articles     Next Articles

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

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.