个人简历

教育经历\r
2003.9 -- 2007.6 北京航空航天大学 工程力学 大学本科毕业 学士学位\r
2007.9 -- 2009.6 北京航空航天大学 飞行器设计 硕士研究生毕业 硕士学位\r
2009.9 -- 2012.12 北京航空航天大学 载运工具运用工程 博士研究生毕业 博士学位\r
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工作经历\r
2020.5 -- 至今 北京航空航天大学 副教授（教研系列） 全职\r
2018.1 -- 2020.5 北京航空航天大学 交通学院飞行器适航工程系 助理教授（教研系列）/研究员 全职\r
2016.7 -- 2017.7 University of Southampton（英国） 工程与环境学院 国家留学基金委公派访问学者\r
2013.1 -- 2017.12 北京航空航天大学 交通学院飞行器适航工程系 讲师 全职\r
2008.9 -- 2012.12 北京航空材料研究院 先进复合材料国防科技重点实验室 联合培养研究生

研究领域

先进复合材料结构力学设计、制备及性能测试表征\r
航天可折叠/展开柔性复合材料结构（弹性大变形、形状记忆大变形、充气展开大变形等）\r
柔性复合材料蒙皮及其航空可变体结构与变体飞机\r
复合材料结构适航\r
编织复合材料本构（2维和3维）\r
复合材料结构损伤失效行为\r
复合材料结构与制备工艺多目标优化设计(遗传算法、神经网络等)""

近期论文

Tian-Wei Liu.Multi-objective optimisation designs for thin-walled deployable composite hinges using surrogate models and Genetic Algorithms.[期刊]:Composite Structures,2022,280:114757\r
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Jiang-Bo Bai,Tian-Wei Liu,Qiu-Hong Lin,Qiang Cong,Yu-Feng Wang,Jiang-Nan Ran,Dong Li,Guang-Yu Bu.Determining the best practice – Optimal designs of composite helical structures using Genetic Algorithms.[期刊]:Composite Structures,2021,268:113982\r
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熊峻江,白江波.平面编织复合材料的飞行器结构力学.[专著].北京:科学出版社\r
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Tian-Wei Liu.An analytical model for predicting compressive behaviour of composite helical Structures: Considering geometric nonlinearity effect.[期刊]:Composite Structures,2021,255:112908\r
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Jiangbo Bai.Micromechanical model for rapid prediction of plain weave fabric composite strengths under biaxial tension.[期刊]:Composite Structures,2020,255:112888\r
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林秋红，白江波，从强. 超长可折叠复合材料豆荚杆轴向压缩屈曲性能测定方法.[期刊]:航空制造技术,2019,62(4):51-54\r
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Folding analysis for thin-walled deployable composite boom.[期刊]:Acta Astronautica,2019,159:622-636\r
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Jiang-Bo Bai, Di Chen, Jun-Jiang Xiong, Chen-Hao Dong. A semi-analytical model for predicting nonlinear tensile behaviour of corrugated flexible composite skin.[期刊]:Composites Part B: Engineering,2019,168:312-319\r
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Jiang-Bo Bai, Chen-Hao Dong, Jun-Jiang Xiong, Chu-Yang Luo, Di Chen. Progressive damage behaviour of RTM-made composite T-joint under tensile loading.[期刊]:Composites Part B: Engineering,2019,160:488-497\r
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Optimal Design of Triaxial Weave Fabric Composites under Tension:Composite Structures,2018,20:616-624\r
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复合材料胶结修补缺损金属结构的力学性能研究:材料工程, 增刊,2009\r
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间隙率对三轴向机织复合材料弹性性能的影响分析:材料工程,2014,3:14-20.\r
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复合材料机翼整体成型技术研究:复合材料学报,2011,28(3):185-191\r
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RTM成型复合材料T型接头工艺参数优化与力学性能实验研究:复合材料学报,2009,26(3):13-17\r
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可折叠复合材料豆荚杆的制备与验证:航空学报,2011,32(7):1217-1223\r
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J.B. Bai, J.J. Xiong, R.A. Shenoi, M. Liu.An analytical model for predicting permanent plastic deflection and strain distributions in aluminium-alloy plates under low velocity impact loading.[期刊]:Proc IMechE Part C: Journal of Mechanical Engineering Science.,2018,232(16):2861–2872\r
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A corrugated flexible composite skin for morphing applications.[期刊]:Composites Part B: Engineerin,2017,131:134-143\r
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Progressive damage modelling of hybrid RTM-made composite Π-joint under four-point flexure using mixed failure criteria:Composite Structures,2017,159::327-334.\r
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Thermal analysis of thin-walled deployable composite boom in simulated space environment:Composite Structures,2017,173:210-218\r
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A micromechanical model for predicting biaxial tensile moduli of plain weave fabric composites:The Journal of Strain Analysis for Engineering Design,2017,52(5):333-343\r
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Analytical solutions for predicting tensile and in-plane shear strengths of triaxial weave fabric composites:International Journal of Solids and Structures,2017,120:199-212\r
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Analytical solutions for predicting tension and shear moduli of triaxial weave fabric composites:Acta Mechanica Solida Sinica,2016,29(1):59-77.\r
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Temperature effect on buckling properties of ultra-thin-walled lenticular collapsible composite tube subjected to axial compression:Chinese Journal of Aeronautics,2014,27:1312-1317.\r
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Simplified analytical model for predicting the temperature of on high-altitude:International Journal of Thermal Sciences,2014,76:82-89.\r
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Analytical solutions for predicting in-plane strain and interlaminar shear stress of ultra-thin-walled lenticular collapsible composite tube in fold deformation:Composite Structures,2013,97:64-75.\r
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Analytical solution for predicting in-plane elastic Shear properties of 2D orthogonal PWF composites:Chinese Journal of Aeronautics,2012,25(4):575-583\r
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Tear resistance of orthogonal kevlar-PWF-reinforced TPU film:Chinese Journal of Aeronautics,2011,24(1):113-118
中国力学学会MTS材料试验协作专业委员会青年委员