• DocumentCode
    2581422
  • Title

    Computer-aided reliability finite element methods

  • Author

    Followell, David A. ; Bocchi, William J. ; Liguore, Salvatore L. ; Perez, Rigo ; Yates, W.D., III

  • Author_Institution
    McDonnell Aircraft Co., St. Louis, MO, USA
  • fYear
    1991
  • fDate
    29-31 Jan 1991
  • Firstpage
    214
  • Lastpage
    221
  • Abstract
    A method that allows simplified linear FEAs (finite-element analyses) to be used instead of the more complex elastic-plastic nonlinear FEA is outlined. Guidelines for mesh generation that will eliminate arithmetic errors caused when materials with large stiffness differences are adjacent to each other are established. The accuracy of FEAs when dealing with very small dimensions was verified. Procedures for combining various loadings in order to predict life are established for materials which exhibit stress relaxation and for those which do not. With these guidelines, FEAs can be used to predict the structural life of electronic equipment
  • Keywords
    engineering computing; failure analysis; finite element analysis; reliability; FEA; FEM; accuracy; electronic equipment; engineering computing; failure analysis; finite element methods; mesh generation; reliability; stiffness differences; stress relaxation; structural life; Aerospace engineering; Aircraft propulsion; Capacitive sensors; Electronic equipment; Fatigue; Finite element methods; Guidelines; Plastics; Reliability engineering; Stress;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1991. Proceedings., Annual
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    0-87942-661-6
  • Type

    conf

  • DOI
    10.1109/ARMS.1991.154438
  • Filename
    154438