Journal of Materials Science

, Volume 43, Issue 20, pp 6599–6603 | Cite as

On the propensity of laminates to delaminate

  • K. H. G. AshbeeEmail author
Stretching the Endurance Boundary of Composite Materials: Pushing the Performance Limits of Composite Structures


Laminates have a propensity to delaminate; the mathematical plane between adjacent plies offers a preferred path for crack propagation, irrespective of the nature of the stress field that gives rise to the elastic strain energy released. This is because the plane between plies is characterised by a specific fracture surface energy significantly lower than those for internal surfaces that intersect fibres. In the second of his two classical publications on fracture, A.A. Griffith showed how crack rotation in two-dimensional stress fields occurs. This suggests how, in a laminate, pre-existing flaws are able to seek out the plane of lamination; here, crack rotation under the influence of, for example, shear stress is examined in the context of laminates designed for use in aerospace. One physical consequence of Griffith’s calculation is the prediction of crack propagation in elastic solids subjected to bidimensional compression with strongly unequal principal stresses. A simple bidimensional compression rig has been devised to investigate this prediction. To obviate the risk of delamination, it will be necessary to move away from anisotropic lay-ups, and further develop three-dimensional weaves and methods for weaving three-dimensional weaves. A method whereby a three-dimensional fibre weave, which has cubic symmetry and no zero-valued shear moduli, might be weaved is outlined.


Principal Stress Uniaxial Compressive Strength Strain Energy Release Elliptic Hole Uniaxial Tensile Strength 



The author gratefully acknowledges correspondence with Dr J. C. Gill, latterly of Bristol University, on the physics of electromagnetic wave propagation by fibre-reinforced materials. The mathematical equations and the figures were prepared with the assistance of T. L. Ashbee.


  1. 1.
    Inglis CE (1913) Trans Inst Nav Archit 55:219Google Scholar
  2. 2.
    Griffith AA (1924) The theory of rupture. In: 1st international conference on applied mechanics, Delft, pp 55–63Google Scholar
  3. 3.
    Orowan E (1948/1949) Rep Prog Phys 12:185. doi: CrossRefGoogle Scholar
  4. 4.
    Ashbee KHG (1991) Bidimensional compression. In: Sir Charles Frank, OBE, FRS: an eightieth birthday tribute. Adam Hilger, pp 353–368Google Scholar
  5. 5.
    Ashbee KHG (1998) Three-dimensional fiber weave with cubic symmetry and no zero-valued shear moduli, US Patent Number 5,804,277Google Scholar
  6. 6.
    Frank FC (1963) ASM Seminar on “Metal Surfaces, Structure, Energetics and Kinetics”, Ch. 1. American Society for MetalsGoogle Scholar

Copyright information

© Springer Science+Business Media, LLC 2008

Authors and Affiliations

  1. 1.ShrewsburyUK

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