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Abstract

When studying failure processes in laminated composites, it is useful to monitor the progression of damage throughout the load history of the material. A variety of test techniques can provide information about damage accumulation, but many of these techniques infer the damage states from some sophisticated interpretation of the raw data. Only two techniques, X-ray radiography and edge replication, give a direct indication of the damage state. The present chapter provides a brief description of edge replication, a technique for the in situ documentation of damage in laminated composites.

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References

  1. Stalnaker, D.O. and Stinchcomb, W.W., “Load History-Edge Damage Studies in Two Quasi-Isotropic Graphite Epoxy Laminates,” Composite Materials: Testing and Design (Fifth Con-ference), ASTM STP 674, ed. S.W. Tsai, ASTM, 620–641 (1979).

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  2. Reifsnider, K.L. and Masters, J.E., “Investigation of Characteristic Damage States in Composite Laminates,” ASME Paper No. 78-WA/Aero-4, Winter Ann. Mtg. (1978).

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  3. Kriz, R.D. and Stinchcomb, W.W., “Effects of Moisture, Residual Thermal Curing Stresses, and Mechanical Load on the Damage Development in Quasi-Isotropic Laminates,” Damage in Composite Materials, ASTM STP 775, ed. K.L. Reifsnider, ASTM, 63–80 (1982).

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  4. Stalnaker, D.O., Kennedy, R.H., and Ford, J.L., “Interlaminar Shear Strain in a Two-Ply Balanced Cord Rubber Composite,” experimental mechanics, 20 (3), 87–94 (1980).

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  5. Highsmith, A.L. and Reifsnider, K.L., “Stiffness-Reduction Mechanisms in Composite Laminates,” Damage in Composite Materials, ASTM STP 775, ed. K.L. Reifsnider, ASTM, 103–117 (1982).

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  6. Johnson, W.S., Lubowinski, S.J., Highsmith, A.L., Brewer, W.D., and Hoogstraten, C.A., “Mechanical Characterization of SCS-6/Ti-15–3 Metal Matrix Composites at Room Temperature,” NASA Tech. Memorandum NASP TM-1014 (April 1988).

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© 1989 Society for Experimental Mechanics

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Highsmith, A.L. (1989). Edge Replication for Laminated Composites. In: Pendleton, R.L., Tuttle, M.E. (eds) Manual on Experimental Methods for Mechanical Testing of Composites. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-1129-1_21

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  • DOI: https://doi.org/10.1007/978-94-009-1129-1_21

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-7000-3

  • Online ISBN: 978-94-009-1129-1

  • eBook Packages: Springer Book Archive

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