Identification of Damage in Composite Structures Using Thermoelastic Stress Analysis

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Abstract:

The application of a cyclic load on a composite material containing damage has the effect of heating due to the material viscoelasticity. This is exaggerated in the proximity of interlaminar failure because of friction between plies. Quantitatively studying a stressed component subject to these conditions using Thermoelastic Stress Analysis (TSA) has been inaccurate, as the localised heating has an effect on the thermoelastic response. Hence the thermoelastic signal from damaging composites will contain a stress-induced component and a temperature-induced component. In this paper a process is described that allows the thermoelastic signal to be de-coupled into a stress component and a temperature component. This is achieved using a combination of infra-red thermography and TSA. The process is based on the use of a special calibration device. The paper provides an experimental verification of the de-coupling using actual damaged composite components.

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Key Engineering Materials (Volumes 293-294)

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583-590

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September 2005

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© 2005 Trans Tech Publications Ltd. All Rights Reserved

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[1] Dulieu-Barton, J. M. and Stanley, P: Journal of Strain Analysis. Vol. 33 (1998), p.93.

Google Scholar

[2] Dulieu-Barton, J.M. Quinn, S. Eyre, C. and Cunningham, P. R: Applied Mechanics and Materials, Vol. 1-2 (2004), p.197.

Google Scholar

[3] Lesniak, J. R. and Boyce, B. R: A High-Speed Differential Thermographic Camera. In Proceedings of Society for Experimental Mechanics Spring Conference, Baltimore (1994).

Google Scholar

[4] Pye, C.J. and Adams, R. D: Heat emission from damaged composite materials and its use in non-destructive testing. J. Phys. D: Appl. Phys. Vol. 14 (1981), p.927.

DOI: 10.1088/0022-3727/14/5/026

Google Scholar

[5] Quinn, S: Thermoelastic stress analysis of oblique holes in flat plates and cylinders. PhD thesis, University of Liverpool. (2000).

Google Scholar

[6] Cunningham, P. R., Dulieu-Barton, J. M., Dutton, A.G. and Shenoi, R. A: Key Engineering Materials. Vol. 204-205 (2001), p.453.

DOI: 10.4028/www.scientific.net/kem.204-205.453

Google Scholar

[7] Nicholas, J.V. and White, D. R: Traceable Temperatures. (Wiley, 2001, second edition).

Google Scholar

[8] Jamieson, J.A., McFee, R.H., Plass, G.N., Grube, R.H. and Richards R. G: Infrared Physics and Engineering. (McGraw-Hill, 1963).

Google Scholar

[9] Jones, R., Heller, M., Lombardo, D., Dunn, S. Paul, J. and Saunders, D: Composite Structures. Vol. 12 (1989), p.291.

Google Scholar

[10] Drew, R.C. and White, R. G: An investigation into damage propagation and its effect upon dynamic properties of CFRP composite materials. Proceedings of the Fourth International Conference on Composite Structures, Paisley College of Technology. (1987).

DOI: 10.1007/978-94-009-3457-3_4

Google Scholar

[11] http: /www. spsystems. com/solutions/solutions_pdfs/pdfs_productdatasheets/prepreg/SE_84. pdf.

Google Scholar