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Volume 25 Issue 5
May  1999
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Journal of Beijing University of Aeronautics and Astronautics  > 1999  >  25(5): 554-557.
Han Haitao, Zhang Zheng, Lu Zixinget al. Differential quadrature solutions for buckling of laminated beams with multiple arbitrary delaminations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(1): 22-25. (in Chinese)
Citation: Xiong Junjiang. Equal Damage Design Method for Fatigue Reliability Design of Structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 554-557. (in Chinese)
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Equal Damage Design Method for Fatigue Reliability Design of Structure

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 23 Apr 1998
  • Publish Date: 31 May 1999
    Abstract
  • The brief development course of fatigue reliability design is reviewed. The concept and principle of equal damage design for fatigue reliability design of structure are proposed. Then the test is carried out in order to validate this design principle, and it is indicated that the parts of a structure designed according to the equal damage design method have the same damage at the given life and break down at the same time. And so it is feasible and easy for the structure to be designed by means of the method presented in this paper, and this method can be conveniently used by the engineers. On the basis of this fatigue reliability design method, the structure may be designed to be safe, reliable and light.

     

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    • References(1)
  • 1. 高镇同. 疲劳应用统计学. 北京:国防工业出版社,1986 2. 高镇同, 熊峻江. 疲劳/断裂可靠性研究现状与展望. 机械强度, 1995, 17(3):61~82 3. Liard F. Fatigue of helicopters-service life evaluation method. AGARD Report, 1978,(674):1~15 4. 熊峻江, 黄新宇, 高镇同,等. 极大似然法对比试验研究及其试验数据处理. 航空学报, 1996, 17(5):539~542 5. 熊峻江, 高镇同. 极大似然法测定的p-S-N曲线的置信度. 北京航空航天大学学报, 1996, 22(6):687~691
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