航空学报 > 1991, Vol. 12 Issue (4): 171-174

短周期谱载荷作用下的疲劳裂纹扩展估算

李玉民   

  1. 沈阳飞机研究所
  • 收稿日期:1989-01-25 修回日期:1989-06-10 出版日期:1991-04-25 发布日期:1991-04-25

THE PREDICTION OF FATIGUE CRACK GROWTH UNDER SHORT PERIOD SPECTRUM LOADIND

Li Yumin   

  1. Shengyang Aircraft Research Institute
  • Received:1989-01-25 Revised:1989-06-10 Online:1991-04-25 Published:1991-04-25

关键词: 载荷间相互影响, 迟滞指数, 塑性区尺寸

Abstract: A semilinear formula in consideration of overload retardation effect is derived from Wheeler's retardation model for the-prediction of fatigue crack growth under short period flight-by-flight or block spectrum loading. As long as the spectrum size is small enough,the result calculated by this formula will closely agree with one of Wheeler's cycle-by-cycle integration.

Key words: load-interaction, retardation exponent, plastic zone size