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Free Edge Stress Fields in Composite Laminates

  • N. J. Pagano
Chapter
Part of the Solid Mechanics and Its Applications book series (SMIA, volume 34)

Abstract

A new theory to predict stress fields within composite laminates is employed to solve the free edge class of boundary value problems. In this theory, the stress field determination reduces to the solution of a one-dimensional problem. The solution involves consideration of 13N algebraic and ordinary differential equations. when N is the number of layers in the laminate. The general solution is valid for an arbitrary number of layers, however, numerical constraints limit the value of N which can be treated by the present approach.

Keywords

Composite Laminate Laminate Thickness Interlaminar Stress Complementary Solution Expansional Strain 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    N. J. Pagano. Stress fields in composite laminates. Int. J. Solids Structures 14. 385–400 (1978).zbMATHCrossRefGoogle Scholar
  2. 2.
    A. H. Puppo and H. A. Evensen, Interlaminar shear in laminated composites. J. Composite Mat. 4, 204 (1970).ADSCrossRefGoogle Scholar
  3. 3.
    R. B. Pipes and N. J. Pagano, Interlaminar stresses in composite laminates under uniform axial extension. J. Composite Mat. 4, 538 (1970).Google Scholar

Copyright information

© Springer Science+Business Media Dordrecht 1994

Authors and Affiliations

  • N. J. Pagano
    • 1
  1. 1.Nonmetallic Materials Division, Air Force Materials LaboratoryWright-Patterson AFBUSA

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