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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2011, Vol. 32 ›› Issue (11): 2036-2041.doi: CNKI:11-1929/V.20110419.1703.007

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Nominal Stress Approach for Life Prediction of Notched Specimens Under Vibration Loading

LI Deyong1,2, YAO Weixing1   

  1. 1. Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicles, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    2. Chengdu Aircraft Design & Research Institute, Chengdu 610041, China
  • Received:2011-01-24 Revised:2011-02-21 Online:2011-11-25 Published:2011-11-24

Abstract: To describe the centralized level of the stress root mean square (RMS) around a notch, this paper proposes a definition and calculation formula of the stress mean square concentration factor for notched specimens under dynamic excitation. A calculation formula for notch fatigue factor is presented based on the basic fatigue mechanism of structures and a consideration of the distribution characteristics of the stress root mean square in dangerous regions around a notch. Consequently the nominal stress approach for the life prediction of notched specimens under vibration loading is obtained. The results of three typical examples show that the method proposed in this paper can predict the vibration fatigue life of notched specimens well.

Key words: vibration fatigue, life prediction, nominal stress approach, stress mean square concentration factor, notch fatigue factor

CLC Number: