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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1991, Vol. 12 ›› Issue (2): 16-21.

• 论文 • Previous Articles     Next Articles

AN EXPERIMENTAL STUDY ON FATIGUE CRACK GROWTH FOR ENGINEERING SMALL CRACKS UNDER ELASTO-PLASTIC CONDITION

Zheng Minzhong, Nie Xuezhou, Liu Xiaoguang   

  1. Aircraft Structure Strength Research Institute
  • Received:1990-06-18 Revised:1990-08-15 Online:1991-02-25 Published:1991-02-25

Abstract: The fatigue crack growth behaviour of engineering small cracks under elasto-plastic condition is studied. The J-integral expression as a main control parameter of fatigue crack growth under elasto-plastic condition is presented.It is suggested that the modified ΔJeft-integral can he used as a main control parameter for engineering cracks in cyclic and plastic area of a notch. The method was verified by the experimental results.

Key words: engineering small crack, elasto-plastic condition, cyclic plastic area of a notch