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陶翀骢
2023-05-11 16:25
  • 陶翀骢
  • 陶翀骢 - 讲师-南京航空航天大学-电子信息工程学院-个人资料

近期热点

资料介绍

个人简历


2018年在南京航空航天大学获得博士学位。一直从事复合材料结构的损伤检测、评估、建模和预测工作,同时也探索新型人工智能算法在传统工程领域的应用,参与国家及省部级项目3项,承担江苏省自然科学基金青年项目等。2016年赴英国布里斯托大学,Bristol Composites Institute(ACCIS)联合培养1年。迄今已发表期刊论文10余篇,其中以第一作者发表SCI收录论文9篇,论文主要集中于Compos. Sci. Tech., Composites Part A, Compos. Struc.等高水平期刊,他引40余次。参与国际会议4次,被ISTP收录会议论文1篇。
教育经历
2012.9 -- 2018.6南京航空航天大学 工程力学 博士研究生毕业 工学博士学位
2008.9 -- 2012.7西北工业大学 工程力学 大学本科毕业 工学学士学位
2005.9 -- 2008.6绍兴市第一中学 普通高中毕业 无学位

研究领域


人工智能技术
复合材料无损检测及剩余性能预测
复合材料损伤建模"复合材料损伤建模和力学能性能预测"

近期论文


[1] 陶翀骢,张超,季宏丽等.On the energy release rate extraction and mixed mode behavior of fatigue cohesive model[J]
[2] 陶翀骢,张超,季宏丽等.Fatigue life prediction of GFRP laminates using averaged Bayesian predictive distribution and Lamb wave velocity[J].Composites Science and Technology
[3] 陶翀骢,张超,季宏丽等.Application of neural network to model stiffness degradation for composite laminates under cyclic loadings[J].Composites Science and Technology
[4] 张超,张振宇,季宏丽等.Mode conversion behavior of guided wave in glass fiber reinforced polymer with fatigue damage accumulation[J].Composites Science and Technology,2020,192
代表性成果:
[1] Tao C, Zhang C, Ji H, et al. Fatigue Failure probability prediction of delamination under cyclic loading in composite laminates using cohesive interface elements[J]. Engineering Fracture Mechanics, 2021, 108064.
[2] Tao C, Zhang C, Ji H, et al. Fatigue damage characterization for composite laminates using deep learning and laser ultrasonic[J]. Composites Part B: Engineering, 2021, 108816.
[3] Tao C, Zhang C, Ji H, et al. Application of neural network to model stiffness degradation for composite laminates under cyclic loadings[J]. Composites Science and Technology, 2021, 203: 108573.
[4] Tao C, Zhang C, Ji H, et al. On the energy release rate extraction and mixed mode behavior of fatigue cohesive model[J]. Composite Structures, 2020, 239: 112038.
[5] Tao C, Zhang C, Ji H, et al. Fatigue life prediction of GFRP laminates using averaged Bayesian predictive distribution and Lamb wave velocity[J]. Composites Science and Technology, 2020: 108213.
[6] Tao C, Mukhopadhyay S, Zhang B, et al. An improved delamination fatigue cohesive interface model for complex three-dimensional multi-interface cases[J]. Composites Part A: Applied Science and Manufacturing, 2018, 107: 633-646.
[7] Tao C, Ji H, Qiu J, et al. Characterization of fatigue damages in composite laminates using Lamb wave velocity and prediction of residual life[J]. Composite Structures, 2017, 166: 219-228.
[8] Tao C, Qiu J, Yao W, et al. A novel method for fatigue delamination simulation in composite laminates[J]. Composites Science and Technology, 2016, 128: 104-115. (IF=7.094)
[9] Tao C, Qiu J, Yao W, et al. The effect of drilling-induced delamination on tensile strength and prediction of residual strength of carbon fiber-reinforced polymer laminate[J]. Journal of Composite Materials, 2016, 50(24): 3373-3384.

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