AC 25.271-1D, Advisory circular-damage tolerance and fatigue evaluation of structure [S]. 2011.
[2]
Bao Rui, Zhang Xiang. Fatigue crack growth behavior and life prediction for 2324-T39 and 7050-T7451 aluminium alloys under truncated load spectra [J]. International Journal of Fatigue, 2010, 32:1180-1189.
[3]
Giancaspro J, Taam W, Wong R. Modified joint weibull approach to determine Load Enhancement Factors [J]. International Journal of Fatigue, 2009, 31: 782―790.
Brandecker B, Hilgert R. A320 full scale structural testing for fatigue and damage tolerance certification of metallic and composite structure [C]. Jerusalem, Israel: Proceedingof 16 ICAS, 1988: 1244―1256.
[6]
杨乃宾. 复合材料飞机结构验证试验载荷放大系数法[J]. 北京航空航天大学学报, 1996, 22(4): 5―10. Yang Naibin. Load enhancement factor of certification testing for composite aircraft structures [J]. Journal of Beijing University of Aeronautics and Astronautics, 1996, 22(4): 5―10. (in Chinese)
[7]
Paris P, Erdogan F A. Critical analysis of crack growth laws[J]. Journal of Basic Engineering, 1963, 85(3): 528―535.
[8]
Walker K. The Effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum [C]. Philadelphia, PA: American Society for Testing and Materials, 1970: 1―14.
[9]
沙宇, 张嘉阵, 白士刚, 周振功. 拉-压循环加载下铝合金疲劳裂纹扩展的压载荷效应研究[J]. 工程力学, 2012, 29(10): 327―334. Sha Yu, Zhang Jiazhen, Bai Shigang, Zhou Zhengong. Study on the effect of compression loading on fatigue crack growth of aluminium under tension-compression cycle [J]. Engineering Mechanics, 2012, 29(10): 327―334. (in Chinese)
[10]
丁振宇, 王效贵, 高增梁. 加载历史和裂纹闭合对疲劳裂纹扩展行为影响的数值模拟[J]. 工程力学, 2013, 30(8): 244―250. Ding Zhenyu, Wang Xiaogui, Gao Zengliang. Numerical simulation of the effect of loading history and crack closure on crack propagation behaviour [J]. Engineering Mechanics, 2013, 30(8): 244―250. (in Chinese)
[11]
Schijve J. Fatigue crack growth predictions for variable-amplitude and spectrum loading [J]. Proc Fatigue, 1987, 87: 1685―720.
[12]
Wheeler O E. Spectrum loading and crack growth [J]. Transaction of the ASME, J Basic Eng, 1972, 3: 181―186.
[13]
Gallagher J P. A generalized development of yield-zone models [R]. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, 1974: 1―12.
[14]
Elber W. The significance of fatigue crack closure, damage tolerance in aircraft structures [C]. West Conshohocken, PA: American Society for Testing and Materials, 1971: 230―242.
[15]
Fu Xiangjion. Prediction of fatigue life with an equivalent damage model [J]. Engineering Fracture Mechanics, 1989, 34: 1241―1248.
[16]
薛景川, 弓云昭, 张茂, 等. 民机民机金属薄壁结构静强度、耐久性/损伤容限综合强度设计和分析研究[J]. 结构强度研究, 2009, 3(65): 1―4. Xue Jingchuan, Gong Yunzhao, Zhang Mao, et al. The integrating strength design and analysis method on stail strength, durability/damage tolerance for civil aircraft metal thin wall structures [J]. Structure and Strength Research, 2009, 3(65): 1―4. (in Chinese)
