The Effect of Hygrothermal Composite Patch on the Fracture of Reinforced Crack under Mixed-Mode Loading

Article Preview

Abstract:

The mechanical properties of composite laminates play a key role in the success of composite reinforcement method, but various investigations suggest that the stiffness of epoxybased composites is sensitive to the variation of moisture ratio and temperature of the working environment. The aim in this research is to characterize the effect of hygrothermal aged composite patch on the strength of repaired cracks, under mixed mode I/II conditions. For this purpose a reinforced sheet, i.e. a crack fastener hole specimen is examined by using a finite element simulation. The crack tip parameters and fracture characteristics of repaired cracks are determined as a function of the total amount of moisture inside the composite patch. The results of this study show that the performance of composite reinforcement technique depends on the amount of water absorption within the bonded patches.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

189-196

Citation:

Online since:

October 2006

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2006 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] A.A. Baker, R.J. Callinan, M.J. Davis, R. Jones and J.G. Williams: Theor Appl Fracture Mech, Vol. 2 (1984), 1-16.

Google Scholar

[2] A.A. Baker: Compos Struct, Vol. 74 (1999), 431-443.

Google Scholar

[3] R. Jones, L. Molent, J. Paul, T. Saunders and W.K. Chiu WK: NASA CP 3274, 1994. p.339350.

Google Scholar

[4] J.M. Gaillardon, H.J. Schmidt and B. Brandecker: NASA CP 3160, 1991. pp.283-289.

Google Scholar

[5] A. Moropoulou, N. Kouloumbi, Z.P. Marioli-Riga, N.P. Avdelidis and P. Pantazopoulou: in Proceedings of Electrically Based Microstructural Characterization III Symposium, Boston, MA, Materials Research Society Press, 2002. pp.39-44.

Google Scholar

[6] A. Bassetti, A. Nussbaumer, P. Colombi,: Advanced FRP Materials for Civil structures, Bologna, Italy, 2000, pp.33-42.

Google Scholar

[7] R. Jones and R.J. Callinan: J Struct Mech., Vol. 7 (1979), 107-130.

Google Scholar

[8] M.R. Ayatollahi and R. Hashemi: Compos Struct, 2006, Article in press.

Google Scholar

[9] A. Megueni, A. Tounsi, B.B. Bouiadjra and B. Serier : Compos Struct , Vol. 62 (2003), 171- 176.

Google Scholar

[10] S. Naboulsi and S. Mall: Compos Struct, Vol. 41 (1998), 303-313.

Google Scholar

[11] G.S. Springer GS. Environmental Effects on Composite Materials, Vol. 2, Thechnomic Publishing Co. Inc., (1984).

Google Scholar

[12] K.H. Ip, P.K. Dutta and D. Hui: Composite: Part B 2001, 599-607.

Google Scholar

[13] ABAQUS Finite Element Program, ABAQUS/Standard 5. 8. Hibbit, Karlsson and Sorensen, Inc. Pawtuket, USA, (1998).

Google Scholar

[14] M.L. Williams: Journal of Applied Mechanics, Vol. 24 (1957), 109-114.

Google Scholar

[15] F. Erdogan and G.C. Sih: Journal of Basic Engng, Vol. 85 (1963), 525-527.

Google Scholar

[16] M.A. Hussain, S.L. Pu and J. Underwood: Fracture Analysis 1974; 560: 2-28.

Google Scholar

[17] Sih GC. Strain energy density factor applied to uniaxial mode crack problems. International Journal of Fracture, Vol. 10 (1974), 305-321.

DOI: 10.1007/bf00035493

Google Scholar

[18] Ayatollahi MR, Aliha MRM. Cracked Brazilian specimen subjected to mode II deformation. Engineering fracture mechnics; 72(4); 2005: 493-503.

DOI: 10.1016/j.engfracmech.2004.05.002

Google Scholar

[19] M.R. Ayatollahi and M.R. M Aliha: Material science and Engineering: A, Vol. 417 (2006), 348-356.

Google Scholar

[20] D.J. Smith, M.R. Ayatollahi and M.J. Pavier: Fatigue Fract Engng Mater Struct., Vol. 24 (2001), 137-150.

Google Scholar

[21] M.R. Ayatollahi, M.J. Pavier and D.J. Smith: International Journal of Fracture, Vol. 91 (1998), 283-298.

Google Scholar

[22] A.H. Sherry, C.C. France and M. R Goldthorpe: Fatigue Fract Engng Mater Struct., Vol. 18 (1995), 141-155.

Google Scholar

[23] B. Hu, J. Gong and G. Verchery : in Proceeding of 11 th conference of the French Society for Composite materials. Arcachon, France, 18-20 November 1998, 255-264.

Google Scholar

[24] P.C. Paris and G.C. Sih: STP381. Philadelphia: ASME 1965. pp.30-83.

Google Scholar

[25] M. Kosai and A.S. Kobayashi: Structural Integrity of Aging Airplanes, 1991, 225-239.

Google Scholar