Issue 48
F. V. Antunes et alii, Frattura ed Integrità Strutturale, 48 (2019) 676-692; DOI: 10.3221/IGF-ESIS.48.64 680 I loading. Different values of and were considered for each of these 24 crack tip positions. The values considered for were 0, 10, 20, 30, 40, 50 and 60º, while for were 0, 10, 20, 30, 40, therefore a total number of 1120 numerical analysis were performed. J integral values (J I and J II ) were obtained for each analysis, from which K I and K II were calculated according: E.J I K I 2 1 υ E.J II K II 2 1 υ (5) Finally, Y I and Y II were obtained using relations 3 and 4. Tabs. B1 and B2 in Appendix B present results obtained for Y I and Y II , respectively, with CosmosM software. Typical variations of geometric factor, Y I , with ( - ), , y and (W/(W-x)) 1.5 can be seen in Figs. 5a, 5b, 5c and 5d, respectively. Maximum values can be observed in Fig. 5a for ( - ) close to zero, which could be expected as zero correspond to pure mode I loading. However, the maximum value is not always zero, which indicates that there are others aspects influencing the geometric factors apart from loading direction. A good fitting is obtained with second order polynomial or sinusoidal function. A second order polynomial also fits well to results in Fig. 5b. It can be seen that the increase of slope at crack tip ( ), keeping all the others parameters fixed, reduces Y I . The typical results presented in Fig. 5c show a linear variation with y. Finally, Fig. 5d shows a linear variation of Y I with (W/(W-x)) 1.5 . This variation is related with the asymmetric geometry of the specimen, which imposes flexure to non-cracked section. The increase of crack length decreases the height of rectangular non-cracked section, and increases flexure moment. The comparison between Figs. 5 indicates that highest variation of Y I occurs with x and then with ( - ). Figure 5 : Variation of Y I with (a) ( ) (for x=52.5 mm; y=0). (b) crack tip slope, ( ) (for x=52.5 mm; y=0). (c) y (for x=37.5 mm; =0º). (d) (W/(W-x)) 1. 5 (for y=0; =10º). A numerical solution with 39 constants was fitted to the numerical results presented in Tab. 4 (Appendix B) and illustrated in Figs. 5: Y I = m. 1.5 (W / (W x)) +b (6) (a) (b) (c) (d)
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