Mode III Interlaminar Fracture in Woven Glass/Epoxy Composite Laminates
Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 32804
Mode III Interlaminar Fracture in Woven Glass/Epoxy Composite Laminates

Authors: Farhad Asgari Mehrabadi, Mohammad Reza Khoshravan

Abstract:

In the present study, fracture behavior of woven fabric-reinforced glass/epoxy composite laminates under mode III crack growth was experimentally investigated and numerically modeled. Two methods were used for the calculation of the strain energy release rate: the experimental compliance calibration (CC) method and the Virtual Crack Closure Technique (VCCT). To achieve this aim ECT (Edge Crack Torsion) was used to evaluate fracture toughness in mode III loading (out of plane-shear) at different crack lengths. Load–displacement and associated energy release rates were obtained for various case of interest. To calculate fracture toughness JIII, two criteria were considered including non-linearity and maximum points in load-displacement curve and it is observed that JIII increases with the crack length increase. Both the experimental compliance method and the virtual crack closure technique proved applicable for the interpretation of the fracture mechanics data of woven glass/epoxy laminates in mode III.

Keywords: Mode III, Fracture, Composite, Crack growth Finite Element.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1332936

Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 2488

References:


[1] Becht G and Gillespie JRJW. Design and analysis of the crack rail shear specimen for mode III interlaminar fracture. Compos Sci Technol. 1988; 31: 143-57.
[2] Donaldson SL. Mode III interlaminar fracture characterization of composite materials. Compos Sci Technol. 1988; 32: 225-49.
[3] Hwang S-F and Hu C-L. Tearing mode interlaminar fracture toughness of composite materials. Polym. Compos. 2001; 22: 57-64.
[4] Sharif F, Kortschot MT, Martin RH. Mode III delamination using a split cantilever beam. In: Martin, R.H. (Ed.), Composite Materials: Fatigue and Fracture. ASTM STP 1230, ASTM, Philadelphia. 1995; 5: 85-99.
[5] Trakas K, Kortschot MT. The relationship between critical strain energy release rate and fracture mode multidirectional carbon fiber/epoxy laminates. In: Armanios, E.A. (Ed.), Composite Materials: Fatigue and Fracture, ASTM STP 1285, ASTM, 1997; 6: 283-304.
[6] Szekrényes A. Improved analysis of the modified split-cantilever beam for mode-III fracture. Int. J. Mech. Sci. 2009; 51: 682-93.
[7] Lee SM. An edge crack torsion method for mode III delamination fracture testing. J Compos Technol Res. 1993; 15: 193-201.
[8] Liao WC and Sun CT. The determination of mode III fracture toughness in thick composite laminates. Compos Sci Technol. 1996; 56: 489-99.
[9] Krueger R. The virtual crack-closure technique: history, approach and applications. ICASE report 2002-10. NASA/CR-2002-211628.