个人简历

2000年毕业于北京航空航天大学飞行器设计与工程专业，获学士学位；2005年毕业于北京航空航天大学固体力学专业，获工学博士学位。2005年1月至2006年12月在北京航空航天大学航空宇航科学与技术博士后流动站从事博士后研究工作；2006年12月留校任教。曾获北京航空航天大学“蓝天新秀”、“蓝天新星（科研）”、北航优秀共产党员称号。\r
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2005年4月-10月在中国一航一飞院上海分院强度室挂职锻炼，参与新支线客机的疲劳分析工作；2006年7月-12月在中国商用飞机公司大型客机联合工程队参与大型客机联合论证工作；2009年2月-2010年1月“国家留学基金委青年骨干教师出国研修项目”在英国Cranfield大学做访问学者。

研究领域

飞机结构疲劳/耐久性，断裂力学/损伤容限，焊接整体结构完整性，飞机结构综合环境长寿命设计与分析评定技术""

近期论文

Xiang Zhang,Rui Bao. Evaluation of the intrinsic crack growth rates of weld joints.International Journal of Fatigue, 33(2011): 588-596.\r
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Yang Hongqin,Bao Rui, Zhang Jianyu, Peng Lei and Fei Binjun. Crack growth behaviour of a nickel-based powder metallurgy superalloy under elevated temperature. International Journal of Fatigue,33(2011):632–641.(Corresponding author)\r
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Yang Hongqin,Bao Rui, Zhang Jianyu, Peng Lei and Fei Binjun. Creep-fatigue crack growth behaviour of a nickel-based powder metallurgy superalloy under high temperature. Engineering Failure Analysis, 18 (2011): 1058–1066. (Corresponding author)\r
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Lei Peng Jianyu Zhang, Libin Zhao,Rui Bao, Hongqin Yang and Binjun Fei. Model I Delamination growth of multidirectional composite laminates under fatigue loading, Journal of Composite Materials, v 45, n 10, p 1077-1090, May 2011\r
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Zhang Jianyu, Shi Xinhong,Bao Rui, Fei, Binjun, Tension-torsion high-cycle fatigue failure analysis of 2A 12-T4 aluminum alloy with different stress ratios, International Journal of Fatigue 33 (2011) 1066–1074.\r
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Rui Bao, X Zhang. An inverse method for evaluation of welding residual stresses via fatigue crack growth test data,Eng Fract Mech, 77(2010): 3143-3156.\r
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Rui Bao, X Zhang. Fatigue crack growth behaviour and life prediction for 2324-T39 and 7050-T7451 aluminium alloys under truncated load spectra,International Journal of Fatigue 32 (2010) 1180–1189.\r
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Rui Bao, Xiang Zhang,Norvahida Ahmad Yahaya.Evaluating stress intensity factors due to weld residual stresses by the weight function and finite element methods.Engng Fract Mech, 77(2010): 2550-2566.\r
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Bao Rui, Zhang Jianyu, Yang Hongqin, Fei Binjun. Stochastic Characteristics of Fatigue Crack Propagation for TA15 Titanium Alloy. Key Engineering Materials Vols. 417-418 (2010) : 873-876.\r
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Jianyu Zhang,Rui Bao, Xiang Zhang, Binjun Fei, A probabilistic estimation method of multiple site damage occurrence for aircraft structures,Procedia Engineering, Volume 2, Issue 1, Fatigue 2010, April 2010, Pages 1115-1124.\r
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Zhang Jianyu,Bao Rui, Fei Binjun.Modified Swift Criteria for Residual Strength of Multiple Site Damage Structure. Key Engineering Materials Vols. 417-418 (2010) pp 881-884.\r
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Li Zhiyong,Bao Rui, Zhang Jianyu, Fei Binjun. Oxidation Study of APS Thermal Barrier Coatings in Elevated Temperatures. MANUFACTURING SCIENCE AND ENGINEERING, PTS 1-5, Advanced Materials Research. VL 97-101, 1546-1549, 2010.\r
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Shi Xinhong, Zhang Jianyu,Bao Rui, Fei Binjun. The Effect of Stress Amplitude on Multi-axial High-cycle Fatigue Failure under Constant Amplitude Loading. Key Engineering Materials Vols. 417-418 (2010) pp 877-880.\r
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Zhang X, Chan B, Lama S, Satikumar V, Shi S,Bao R, Influence of impact dents on the fatigue strength of aluminium alloy friction stir welds,Procedia EngineeringVolume 2, Issue 1, Fatigue 2010, April 2010, Pages 1691-1700.\r
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时新红,张建宇,鲍蕊,费斌军.比例加载下应力幅比对 2A12-T4疲劳寿命的影响.北京航空航天大学学报. 2010,36(8):965-968.\r
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时新红,张建宇,鲍蕊,费斌军.拉扭复合加载下相位差对 2A12-T4铝合金高周疲劳失效的影响.航空材料学报. 2010, 30(5):93-96.\r
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李志永,张建宇,鲍蕊,胡浩炬,费斌军. TBCs热应力影响因素的正交有限元分析.北京航空航天大学学报. 2010,36(11):1339-1342.\r
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T. Zhang,R. Bao, P. Liu, B. Fei. Study on Crack Branching of 2324-T39 Aluminum Alloy under Tension Dominated Spectrum Loading. Proceedings of the 12th International Conference on Aluminium Alloys, September 5-9, 2010, Yokohama, Japan 2010. The Japan Institute of Light Metals,pp. 332-337.\r
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杨洪琴，鲍蕊，钱秀清，费斌军.温度/交变载荷作用下裂纹扩展模型及其参量确定，机械强度，32(4)，2010：651-655.\r
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Tian Hailing,Bao Rui, Zhang Jianyu, Zheng Xiaoling, Fei Binjun. The Influence of Low Load Truncation Level on Crack Growth for Al 2324-T39 and Al 7050-T7451. Chinese journal of aeronautics, 22(3): 401-406, 2009. (corresponding author)