Issue 42

D. Rozumek et alii, Frattura ed Integrità Strutturale, 42 (2017) 23-29; DOI: 10.3221/IGF-ESIS.42.03 26 relationship between lengths of cracks is: a/c = 0.274, whereas for ratio R = 0 and c = 7.20 mm this relationship is: a/c = 0.174. The results of crack length measurements a = f (c) show higher curvatures for ratio R = -1 than for R = 0. Fig. 5b presents experimental test results performed for the same specimen as in Fig. 5a, but for further through crack growth. Figs. 5a and 5b demonstrate in diagrams non-uniform fatigue cracks growth on both specimen active side and passive side. Higher crack growth values were measured for active side than passive side. Test results (Fig. 5b) allowed observing that for load ratio R = -1 and crack length a = 7.10 mm, the relationship a/a* = 1.203 has higher values than for the ratio R = 0, where a/a* = 1.092. Whereas, for R = -1 and a* = 0.15 mm, the relationship a/a* = 14.333 also has higher values than for the ratio R = 0, which is a/a* = 10.133. We may also observe that for a* = 0.15 mm the relationship a/a* is approximately twelve times (R = -1) and nine times higher (R = 0) than for a = 7.10 mm. Moreover, experimental test results shown in Fig. 5b allow observing that during the final cracking stage, the lengths of cracks on the sides active and passive, for R = 0, are close to each other, and for R = - 1 the difference between these lengths is higher. a) b) Figure 5 : Fatigue crack length under bending with torsion for: a) cracks edge quarter-elliptic, b) through cracks on both specimen sides: active and passive. Figure 6 : Fatigue crack length „a” versus number of cycles N (active side specimen).