78 / 2021-03-31 16:50:38
A multiaxial fatigue life prediction method for metallic material under combined random vibration loading and mean stress loading in the frequency domain
multiaxial random stress,critical plane criterion,spectral method,mean stress effect,random vibration fatigue experiment
Draft Pending
代阳 高 / 南京航空航天大学
A spectral method for the determination of the critical plane is proposed for metallic material under random vibration loadings based on the criterion of maximum shear stress amplitude, where the direction of critical plane is obtained by solving the maximum value of a function using mathematical optimization method and the fatigue critical location of the structure can be determined. A multiaxial fatigue damage parameter is proposed for combined random vibration loading and mean stress loading cases based on Susmel’s criterion, which is a Power Spectral Density(PSD) of the equivalent shear stress and can be adopted for fatigue life evaluation. The fatigue life estimation of structures under multiaxial random vibration loadings with mean stresses in the frequency domain could be carried out based on this damage parameter constructed at the fatigue critical location with the spectral method for random vibration fatigue life. The multiaxial random vibration fatigue experiment with mean stress loadings is conducted on the notched plate specimens made of 2297-T87 aviation grade aluminum alloy, and the initiation sites of the fatigue cracks as well as the experimental fatigue lives are compared with those calculated by the proposed models, where satisfactory prediction capabilities on both the fatigue crack initiation locations and fatigue lives of the models are demonstrated.
Important Date
  • Conference Date

    May 21

    2021

    to

    May 23

    2021

  • Apr 13 2021

    Abstract Submission Deadline

  • Apr 30 2021

    Abstract Notification of Acceptance

  • Apr 30 2021

    Final Paper Deadline

  • Jun 05 2021

    Registration deadline

Sponsored By
中国力学学会固体力学专业委员会
Organized By
华中科技大学航空航天学院
工程结构分析与安全评定湖北省重点实验室
《固体力学学报》编辑部