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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1989, Vol. 10 ›› Issue (11): 609-612.

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THE SIMULATION OF DYNAMIC CRACK PROPAGATION IN DCB MODEL BY QUASI-STATIC “MOVING SINGULAR ELEMENT METHOD”

Wen Jian1, Liu Yuanyong2   

  1. 1. Aircraft Structural Strength Research Institute;2. Northwestern Polytechmcal University
  • Received:1988-09-01 Revised:1900-01-01 Online:1989-11-25 Published:1989-11-25

Abstract:

In this paper, a modified “Moving Singular Element Method” is presented by using a new variational equation in place of “energy-consistent variational statement”, which is more rigorous in theoretic concept and more convenient to perform. Furthermore, on the basis of it, a so-called “Quasi-static Moving Singular Element Method” is shown, which takes about 50% less CPU time when actually computing and has a reasonable accuracy.

Key words: singular element, dynamic crack propagation, dynamic crack propagating toughness