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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2003, Vol. 24 ›› Issue (3): 234-236.

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Research on Fatigue Damage Cumulative Rule under Corrosion Environment

YANG Xiao-hua1,2, YAO Wei-xing1, DUAN Cheng-mei2   

  1. 1. Faculty 102; Nanjing University of Aeronautics and Astronautics; Nanjing 210016; China;2. Qingdao Branch; Naval Aeronautical Engineering Academy; Qingdao 266041; China
  • Received:2002-07-29 Revised:2002-11-08 Online:2003-06-25 Published:2003-06-25

Abstract: Tests of LC4 aluminum fatigue damage cumulative under / fatigue( 1) + cor rosion+ fat igue( 2)0 mode havebeen car ried out. The test results show that equal level loading tests under the mode have an analogy wit h / lowhigh0 two level loading tests under gener al condit ions. Preceding loading has a for ging effect of low loading on thefatigue behavior of behind loading. Hence, this paper presents a damage cumulat ive hysteretic model. The predictedresults of the damage cumulative hysteretic model and the test results mode ar e in good agreement.

Key words: environment, calendar life, fatigue damage, damage accumulation, corrosion, hysteretic model

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