Issue 35

S. Glodež et alii, Frattura ed Integrità Strutturale, 35 (2016) 152-160; DOI: 10.3221/IGF-ESIS.35.18 158 direction. The final computational results are presented in Tabs. 2 and 3, while the crack path is shown in Fig. 9, where scale factor 10 is used. It is evident from Fig. 9, that complete fracture of upper left half structure is expected after cross section No. 7 will be broken. The appropriate total number of stress cycles N according to Eq. (1) can then be assumed as a total fatigue life of treated structure. Figure 8 : Numbering of critical cross sections Cross section No. Von Mises equivalent stress  M [MPa] Total strain amplitude  a [MPa] Crack initiation period N i [cycles] Initial crack length a i [mm] 1 350 0.0110 472 0.05 2 378 0.0229 110 0.03 3 344 0.0136 307 0.03 4 336 0.0121 387 0.03 5 327 0.0108 489 0.03 6 326 0.0200 495 0.03 7 304 0.0090 731 0.03 Table 2 : Computational results for the crack initiation period. C ONCLUSIONS he computational fatigue strength investigation in respect to the crack initiation and crack propagation in dynamic loaded lotus-type porous structure made of nodular cast iron is presented in this paper. The crack initiation period, N i , has been determined using strain life approach with consideration of simplified universal slope method T No.1 No.2 No.3 No.4 No.5 No.6 No.7