A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions

Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to in...

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Published inComposites science and technology Vol. 64; no. 3; pp. 449 - 476
Main Authors Kaddour, A.S., Hinton, M.J., Soden, P.D.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.03.2004
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Abstract Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to include five more theories, supplied by their originators. Evaluation of the predictive capabilities of the additional theories was carried out in an identical manner to the original study. The same test cases were utilised, covering a wide range of lay-ups, materials and in-plane loading conditions. The results (initial and final failure envelopes and representative stress–strain curves) have been superimposed to show similarities and differences between the predictions of the 19 theories. Final failure predictions for the additional theories fall within the existing range obtained from the original 14 theories but the initial failure predictions for the additional theories have widened the previously observed range. Comments are provided on the possible reasons for the increased spread.
AbstractList Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to include five more theories, supplied by their originators. Evaluation of the predictive capabilities of the additional theories was carried out in an identical manner to the original study. The same test cases were utilised, covering a wide range of lay-ups, materials and in-plane loading conditions. The results (initial and final failure envelopes and representative stress–strain curves) have been superimposed to show similarities and differences between the predictions of the 19 theories. Final failure predictions for the additional theories fall within the existing range obtained from the original 14 theories but the initial failure predictions for the additional theories have widened the previously observed range. Comments are provided on the possible reasons for the increased spread.
Author Kaddour, A.S.
Soden, P.D.
Hinton, M.J.
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  article-title: Predictions of a generalised maximum-shear-stress failure criterion for certain fibrous composite laminates
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(97)00193-0
  contributor:
    fullname: Hart-Smith
– volume: 58
  start-page: 1045
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB9
  article-title: Failure analysis of FRP laminates by means of physically based phenomenological models
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00140-6
  contributor:
    fullname: Puck
– volume: 58
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  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB2
  article-title: Lamina properties and lay-up configurations and loading conditions of a range fibre reinforced composite laminates
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(98)00078-5
  contributor:
    fullname: Soden
– volume: 58
  start-page: 1083
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB10
  article-title: Prediction of laminate failure with Rotem failure criterion
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00143-1
  contributor:
    fullname: Rotem
– volume: 58
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  article-title: Failure criteria for use in the design environment
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00144-3
  contributor:
    fullname: Eckold
– volume: 58
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  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB15
  article-title: Comparison of the predictive capabilities of current failure theories for composite laminates
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(98)00077-3
  contributor:
    fullname: Soden
– volume: 58
  start-page: 1043
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB5
  article-title: Stress based Grant-Sanders method for predicting failure of composite laminates
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00139-X
  contributor:
    fullname: Edge
– volume: 58
  start-page: 1001
  year: 1998
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  article-title: Predicting failure in composite laminates
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(98)00074-8
  contributor:
    fullname: Hinton
– ident: 10.1016/S0266-3538(03)00226-4_BIB19
– ident: 10.1016/S0266-3538(03)00226-4_BIB20
– volume: 62
  start-page: 1515
  year: 2002
  ident: 10.1016/S0266-3538(03)00226-4_BIB16
  article-title: Expanding the capabilities of the ten-percent rule for predicting the strength of fibre-polymer composites
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(02)00092-1
  contributor:
    fullname: Hart-Smith
– ident: 10.1016/S0266-3538(03)00226-4_BIB17
– ident: 10.1016/S0266-3538(03)00226-4_BIB18
– volume: 58
  start-page: 1137
  year: 1998
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  article-title: Prediction of composite laminate fracture
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(97)00014-6
  contributor:
    fullname: Gotsis
– volume: 58
  start-page: 1069
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB6
  article-title: Predicting transverse crack formation in cross-ply laminate
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00142-X
  contributor:
    fullname: McCartney
– volume: 58
  start-page: 1023
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB12
  article-title: A progressive quadratic failure criterion of a laminate
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00141-8
  contributor:
    fullname: Liu
– ident: 10.1016/S0266-3538(03)00226-4_BIB21
– volume: 58
  start-page: 1107
  year: 1998
  ident: 10.1016/S0266-3538(03)00226-4_BIB13
  article-title: A strain energy based failure criterion for nonlinear analysis of composite laminates subjected to biaxial loading
  publication-title: Compos Sci Tech.
  doi: 10.1016/S0266-3538(96)00145-5
  contributor:
    fullname: Wolfe
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Snippet Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14...
Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225-54, 1998), which compared the predictions of 14...
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SubjectTerms B. Stress–strain curves
Failure criteria
Multiaxial failure envelopes
Title A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions
URI https://dx.doi.org/10.1016/S0266-3538(03)00226-4
https://search.proquest.com/docview/28114784
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