一、基本信息 

毕业院校：南京航空航天大学

学历：工学博士学位

所在单位：直升机动力学全国重点实验室/直升机研究院

联系方式：yangtao-007@nuaa.edu.cn

南京航空航天大学直升机动力学全国重点实验室/直升机研究院，博士后（助理研究员），2013年以来一直在南京航空航天大学学习，获飞行器设计专业工学博士学位。长期从事直升机计算流体力学，计算气动声学，高精度数值离散格式等研究。主持直升机动力学全国重点实验室基金、空天飞行空气动力科学与技术全国重点实验室基金等项目，以第一作者在《Journal of Computational Physics》、《Aerospace Science and Technology》、《Computers and Fluids》、《Applied Acoustics》、《International Journal for Numerical Methods in Fluids》等著名学术期刊上发表SCI论文6篇，授权发明专利4项。

二、主要论文与发明专利：

(1) Tao Yang, Guoqing Zhao, Qijun Zhao. Novel TENO schemes with improved accuracy order based on perturbed polynomial reconstruction. Journal of Computational Physics, 2023

(2) Tao Yang, Yan Ding, Xi Chen, Qijun Zhao. Numerical investigation on the blade vortex interaction noise reduction using higher harmonic control. Aerospace Science and Technology, 2024.

(3) Tao Yang, Dazhi Sun, Qijun Zhao, Guoqing Zhao, Xi Chen. Perturbed polynomial reconstructed seventh-order hybrid WENO scheme with improved accuracy and resolution. Computers and Fluids, 2025.

(4) Tao Yang, Xi Chen, Qijun Zhao, Yan Ding. Numerical analysis on the high-speed impulsive noise propagation characteristic of helicopter rotor in the presence of strong shear flow. Applied Acoustics, 2023.

(5) Tao Yang, Xi Chen, Bo Wang, Qijun Zhao, Guoqing Zhao. Perturbed polynomial with multiple free-parameters reconstructed WENO schemes. International Journal for Numerical Methods in Fluids, 2024.

(6) Tao Yang, Xi Chen, Qijun Zhao, Guoqing Zhao. Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield based on linearized Euler equations. International of Aeroacoustics, 2022.

(7) 王博, 杨涛, 招启军, 林沐阳, 杜思亮, 陈希, 赵国庆, 张夏阳. 一种机翼构型及倾转旋翼机. 专利号：CN202111042849.1. (授权)

(8) 招启军, 杨涛, 陈希, 王博, 赵国庆. 一种旋翼噪声确定方法及系统. 专利号：CN202010363696.X. (授权)