13th International Conference on Fracture June 16–21, 2013, Beijing, China -10- [14] Chen Long, Cai Lixun, Yao Di, 2012. A new method to predict fatigue crack growth rate of materials based on average cyclic plasticity strain damage accumulation. Chinese Journal of Aeronautic. (in press) [15] Schwalbe, K.H., 1974. Comparison of several fatigue crack propagation laws with experimental results. Engineering Fracture Mechanics. 6(2): 325-341. [16] Green, A.,.E., John, E., Srawley, 1965. Stress-intensity factors for single-edge-notch specimens in bending or combined bending and tension by boundary collocation of a stress function. NASA TN D-2603. [17] Newman,J.C. Jr., 1976. Predicting failure of specimens with either surface cracks or corner cracks at holes. NASA TN D-8244. [18] Putra, I.S,, Schijve, J., 1992. Crack opening stress measurements of surface cracks in 7075-T6 aluminum alloy plate specimen through electron fractography. Fatigue Fract Engng Mater Struct, 15(4):323-338. [19] Noroozi A.H., Glinka, G.., Lambert, S., 2005. A two parameter driving force for fatigue crack growth analysis. International Journal of Fatigue. 27(10-12): 1277-1296. [20] Wu Zhixue, 2007. Numerical simulation to surface crack fatigue growth(II)[J]. Chinese Journal of Applied Mechanics. 24(1):42-47.(in Chinese) . [21] Brennan, F.P., Ngiam, S.S., Lee, C.W., 2008. An experimental and analytical study of fatigue crack shape control by cold working. Journal of Engineering Fracture Mechanics. 75(3-4):355-363.
RkJQdWJsaXNoZXIy MjM0NDE=