Aviation Industry Science and Technology Commission. The aircraft structural damage tolerance design guidelines [M]. Beijing: Aviation Industry Science and Technology Information Research Institute Press, 1985: 49―470. (in Chinese)
[3]
Jones R, Peng D, Chaperon P, et al. Structural optimization with damage tolerance constraints [J]. Theoretical and Application Fracture Mechanics, 2005, 43(1): 133―155.
Li Shanshan, Xing Lingge, Ding Huiliang, Duan Shihui. Research on damage tolerance design optimization in aircraft structure preliminary design optimization [J]. Advances in Aeronautical Science and Engineering, 2011, 2(1): 79―83. (in Chinese)
Cai Ling, Huang Qiqing, Yin Zhiping, Xie Wei. Optimum design based on damage tolerance for integrated wing-beam structure [J]. Journal of Mechanical Strength, 2009, 31(4): 620―624. (in Chinese)
Zhan Fuyu. Damage tolerance analysis and design for fillet crack in the fuselage opening [D]. Xi’an: Northwestern Polytechnical University, 2012. (in Chinese)
Jiang Jinfeng, Zhang Yin, Sun Qin. Global/Local analysis for progressive fracture of bolted structure [J]. Journal of Nanjing University of Aeronautics & Astronautic, 2010, 42(3): 318―321. (in Chinese)
Yan Ziwan, Hou Chi. Strength analysis approach for multi-bolt joints based on submodeling technique [J]. Advances in Aeronautical Science and Engineering, 2011, 2(4): 419―424. (in Chinese)
