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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1995, Vol. 16 ›› Issue (2): 99-103.

• 论文 • Previous Articles     Next Articles

CHARACTERISTIC STRESS APPROACH FOR DURABILITY ANALYSIS

Wang Zhizhi, Nie Xuezhou, Zheng Minzhong   

  1. Aircraft Structure Strength Research Institute,Xi'an, 710061
  • Received:1994-06-14 Revised:1944-09-27 Online:1995-04-25 Published:1995-04-25

Abstract: The a-s-N curve expressed by characteristic stress of structural details is presented. Then the ( a K ,N K ) data under constant loading are transformed into the ( a K ,t K ) data under spectrum loading by using Goodman diagram and Miner's rule,and equivalent initial flaw size (EIFS) distribution parameters are obtained by the ( a K ,t K ) data.Finally,the probability of crack exceedance and structural damage degree are calculated and the durability analysis is completed.

Key words: durability, distribution parameters systems, crack

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