PSI - Issue 22

Yang Ai et al. / Procedia Structural Integrity 22 (2019) 70–77

77

8

Y. Ai et al. / Structural Integrity Procedia 00 (2019) 000 – 000

loading,” Eng. Fract. Mech. , vol. 75, no. 3 – 4, pp. 534 – 550, 2008. [21] C. Przybilla, A. Fernández- Canteli, and E. Castillo, “An iterative method to obtain the specimen -independent three-parameter Weibull distribution of strength from bendi ng tests,” Procedia Eng. , vol. 10, pp. 1414 – 1419, 2011. [22] X. Pengpeng, H. Xuteng, and S. Yingdong, “LCF life prediction for TC4 alloy notched specimens based on theory of critical dis tance,” J. Aerosp. Power , vol. 5, 2012. [23] W. Illg, “Fatigue tests o n notched and unnotched sheet specimens of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel with special consideration of the life range from 2 to 10,000 cycles,” Natl. Advis. Comm. Aeronaut. , 1956.