Experimental Determination of the Crack Tip Stress Intensity Factor in Integrally Stiffened Panels

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Integral structures offer large benefits in terms of manufacturing cost, but suffer from a lower degree of fail safety when compared to built-up structures. In order to achieve an improvement on the fatigue crack propagation (FCP), crack containment features (also known as crenellations) have been used on these structures. The source of the FCP improvement is the stress intensity factor (K) modification due to the geometry change. In the current study, an analysis about means of estimating K from the experimental information, and also to verify the K behavior while the crack propagates was performed. The study tested two AA 7475 panels, one with crenellations and another without. As the crack propagates, the K values were estimated in two forms, based on the crack propagation rate and by using a digital image correlation (DIC) system, coupled with strain gages. Based on DIC system, it was possible to evaluate the K estimation, the singularity dominated zone size and the K increase, as long as the crack propagated, for both test specimens. A comparison between the two methods was also made, and finally the use of a DIC system as a tool for estimating the K parameter was discussed.

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112-127

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January 2016

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© 2016 Trans Tech Publications Ltd. All Rights Reserved

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[1] Uz, M.V. and Chen, Y.J. and Huber, N. In: Fatigue Life Improvement of Metallic Aerospace Structures via Crenellations, Proceedings of the 26th ICAF Symposium, Komorowski, J. (Ed. ), Montreal.

DOI: 10.1007/978-94-007-1664-3_63

Google Scholar

[2] Ehrström, J.C. and Veen, S.V.D. and Arsène, S. and Muzzolini, R. In: Improving Damage Tolerance of Integrally Machined Panels, Proceedings of the 23rd ICAF Symposium, Donne, C. D. (Ed. ), Hamburg.

Google Scholar

[3] Poe, C.C., Jr., (1971). Damage Tolerance in Aircraft Structures, ASTM STP 486, American Society for Testing and Materials, pp.79-97.

Google Scholar

[4] Anderson, T.L., (1995). Fracture Mechanics Fundamentals and Applications, CRC Press, pp.25-101.

Google Scholar

[5] Sutton, M.A. and McNeil, S.R. and Helm, J.D. and Chao, Y. J, (2000). Photomechanics, P.K. Rastogi, New York pp.323-372.

Google Scholar

[6] Sutton, M.A. and Orteu, J.J. and Schreier H.W., (2009). Image Correlation for Shape, Motion and Deformation Measurements, Springer Science+Business Media.

DOI: 10.1007/978-0-387-78747-3

Google Scholar

[7] Siebert, T. and Crompton, M. J. In: Application of High Speed Digital Image Correlation for Vibration Mode Shape Analysis, Proceedings of the SEM annual Conference 2010, Indianapolis, USA.

Google Scholar

[8] Jr, J.M.F. In: Medição de Deformações em Ensaios Estruturais e Materiais Através de Sistemas Ópticos, Proceedings of the 2nd EMBRAER Technology and Innovation Seminar, Brazil.

Google Scholar