2012年毕业于西北工业大学，2018年获南京航空航天大学工程力学博士学位，同年入职航空学院智能所。研究方向为复合材料的破坏断裂和疲劳以及结合无损检测技术的复合材料力学性能预测方法。

代表性科研成果

期刊论文

（1）Tao C, Qiu J, Yao W, et al. A novel method for fatigue delamination simulation in composite laminates[J]. Composites Science & Technology, 2016, 128:104-115, IF:4.873, SCI一区

（2）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, 2018, 107: 633-646, IF:4.075, SCI一区

（3）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, IF:3.858, SCI二区

（4） Tao C, Qiu J, Yao W, et al. The effect of drilling-induced delamination on tensile strength and prediction of residual strength of CFRP laminate[J]. Journal of Composite Materials, 2016, 50:3373-3384, IF:1.494, SCI三区

会议论文

（1） Tao C, Qiu J.Fatigue Life Prognosis for Composite Laminates Using Lamb Wave Velocity [C]//22nd International Conference on Composite Materials, 2019

（2） Tao C, Qiu J. Prediction of Fatigue Life of Composite Laminates Using Laser Ultrasonic Method[C]//21st International Conference on Composite Materials, 2017

（3）Tao C, Qiu J. A Lamb wave velocity degradation model for cross-ply laminates under fatigue loading[C]// 43rd Review of Progress in Quantitative Nondestructive Evaluation, 2017:090003.

（4） Tao C, Qiu J, Yao W, et al.A Mesh Independent FE Model for Simulation of Delamination under Fatigue Load[C]// 2nd China International Congress on Composite Materials, 2015

（5） Tao C, Qiu J, Yao W, et al. Numerical Investigation of Effect of Drilling-induced Delamination on Fatigue Life of Open Holed Composite Laminate[C]//1st NUAA-Tohoku University Joint Symposium on Fluid Science, Aerospace Engineering and Smart Structure Technology, 2015

（6） Tao C, Qiu J, Okabe T, et al. Effects of Delamination on Strength of Drilled CFRP[C]// International Conference on Flow Dynamics. 2014.