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. Author manuscript; available in PMC: 2009 Jun 25.
Published in final edited form as: Acta Mater. 2007 Apr 1;55(7):2479–2488. doi: 10.1016/j.actamat.2006.11.042

Fig. 7.

Fig. 7

Number of cycles nF to contact-induced veneer failure from O and I cone cracks vs. core failure from R radial cracks, for glass/alumina/polycarbonate trilayers, as a function of maximum contact load Pm. The lines are from Figs. 4 and 5, data omitted.