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
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