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Further Study of Composite Laminates Under Cylindrical Bending

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

Abstract

In a series of three papers [1,2,3], the range of applicability of classical laminated plate theory (CPT) in describing the response of composite laminates under static bending has been examined. Briefly, exact solutions within the framework of linear elasticity theory were developed and compared to the respective solutions governed by CPT [4,5,6]. Numerical data calculated based on simple harmonic load distributions have indicated rather wide discrepancy between the two solutions for laminates having low span-to-depth ratios. At high aspect ratios however, the CPT solution is in good agreement with the elasticity solution.

Keywords

High Aspect Ratio Composite Laminate Concentrate Load Sandwich Plate Elasticity Solution 
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References

  1. 1.
    N. J. Pagano, “Exact Solutions for Composite Laminates in Cylindrical Bending,” J. Composite Materials, Vol. 3 (1969), p. 398.ADSCrossRefGoogle Scholar
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    N. J. Pagano, “Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates,” J. Composite Materials, Vol. 4, (1970), p. 20.Google Scholar
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    N. J. Pagano, “Influence of Shear Coupling in Cylindrical Bending of Anisotropic Laminates,” J. Composite Materials, Vol. 4 (1971), p. 330.MathSciNetADSCrossRefGoogle Scholar
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    S. B. Dong, K. S. Pister and R. L. Taylor, “On The Theory of Laminated Anisotropic Shells and Plates,” J. Aero. Sci., Vol. 28 (1962), p. 969.Google Scholar
  7. 7.
    N. J. Pagano and A. S. D. Wang, “Further Study of Unidirectional and Bidirectional Composites Under Cylindrical Bending,” Air Force Materials Laboratory Report, AFML-TR-71- (1971).Google Scholar

Copyright information

© Springer Science+Business Media Dordrecht 1994

Authors and Affiliations

  • N. J. Pagano
    • 1
  • A. S. D. Wang
    • 2
  1. 1.Air Force Materials LaboratoryWright-Patterson AFBUSA
  2. 2.Drexel UniversityPhiladelphiaUSA

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