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的个人主页 http://shi.buaa.edu.cn/liubinchao1/zh_CN/index.htm
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[1] 施英杰,刘斌超,鲁嵩嵩,陈亮,尚海,鲍蕊.融合“试验-仿真”标定数据的机翼应变载荷关系神经网络模型:航空学报
[2] Binchao LIU,Rui BAO,Songsong Lu.Effects of gas-pore sizes and locations on fatigue failure: A peridynamic study:Theoretical and Applied Fracture Mechanics,2024
[3] Qiuyi Wang,Rui Bao,Binchao Liu,Hui Peng,Songsong Lu,Bo Chen.Comparison of fatigue crack growth behaviour in electron-beam and laser powder-bed-fusion Inconel 718:Materials Science & Engineering A,2024
[4] Kai Wang,Binchao Liu,Qiuyi Wang,Rui Bao.Macrostructures and mechanical properties in laser melting deposited titanium alloy plate at different thickness positions:Materials Science & Engineering A,2022
[5] 刘斌超,王秋懿,杨蓉,鲁嵩嵩,鲍蕊.材料因素对金属疲劳裂纹扩展的影响:航空科学技术,2022
[6] Binchao Liu,Bocai Chen,Songsong Lu,Qiuyi Wang,Rui Bao.Investigations into Gas-Pore Effects on Fatigue Strength with a Peridynamic Approach:Aerospace,2022
[7] Binchao LIU,Rui BAO,Fucheng SUI.A fatigue damage-cumulative model in peridynamics:Chinese Journal of Aeronautics,2021
[8] 刘斌超,鲍蕊,隋福成.一种引入材料循环本构的单轴疲劳平均应力模型:航空学报,2021
[9] Binchao Liu,Kai Wang,Rui Bao.The effects of α/β phase interfaces on fatigue crack deflections in additively manufactured titanium alloy: A peridynamic study:International Journal of Fatigue,2020
[10] Binchao Liu,Zhongwei Yang,Rui Bao.The grain orientation effects on crack-tip fields for additively manufactured titanium alloy: A peridynamic study:Theoretical and Applied Fracture Mechanics,2020

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