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Fatigue Damage Analysis of Notched Carbon/Epoxy Composite by Spate and Finite Element Method

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Developments in the Science and Technology of Composite Materials

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Abstract

Damage-threshold analysis of notched [0/90]2s and [90/0]2s carbon/epoxy laminates is carried out by using thermoelastic technique (SPATE) and a three dimensional finite element method. Fatigue strength and damage extension is examined experimentally and the process of transverse lamina cracking is analyzed numerically in the framework of Linear Elastic Fracture Mechanics.

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References

  1. - O’Brien, T. K., NASA Tech. Memorandum, 100548 (1988).

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  2. - Webber, J. M. B., Proc. 1st Int. Conf. Stress Analysis by Thermoelastic Technique, (1984), 1–8.

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  3. - Kageyama, K., Ueki, K. and Kikuchi, M., Proc. VI Int. Congr. Exp. Mech., (1988), 931.

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  4. - Kitagawa H. et al., Trans. JSME, Ser. A, 50–450 (1984), 129.

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Author information

Authors and Affiliations

  1. University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, 113 Tokyo, Japan

    K. Kageyama

  2. Science University of Tokyo, Noda - Chiba 278, Japan

    M. Kikuchi

  3. Mechanical Engineering Lab., Tsukuba, Ibaraki 305, Japan

    K. Nonaka

Authors
  1. K. Kageyama
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  2. M. Kikuchi
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  3. K. Nonaka
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Editor information

Editors and Affiliations

  1. DLR, Germany

    J. Füller , G. Grüninger  & K. Schulte ,  & 

  2. EACM, USA

    A. R. Bunsell  & A. Massiah  & 

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© 1990 Elsevier Science Publishers Ltd

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Kageyama, K., Kikuchi, M., Nonaka, K. (1990). Fatigue Damage Analysis of Notched Carbon/Epoxy Composite by Spate and Finite Element Method. In: Füller, J., Grüninger, G., Schulte, K., Bunsell, A.R., Massiah, A. (eds) Developments in the Science and Technology of Composite Materials. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-0787-4_25

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  • DOI: https://doi.org/10.1007/978-94-009-0787-4_25

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-6841-3

  • Online ISBN: 978-94-009-0787-4

  • eBook Packages: Springer Book Archive

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