一、基本信息

南京航空航天大学直升机研究院讲师，主要从事直升机旋翼流场数值模拟方法、直升机气动、噪声主动控制、优化评估与分析等研究。以第一/通讯作者发表SCI论文10余篇，授权专利/软著10多项，并获江苏省“卓越博士后”计划资助。目前主持国家重点实验室基金，中国博士后科学基金，参与自然科学基金、基础加强计划重点项目等多个国家级项目，相关科研成果获省部级奖项两项。

二、教育经历

(1) 2015-09 至 2021-06, 南京航空航天大学, 飞行器设计, 博士

(2) 2011-09 至 2015-06, 南京航空航天大学, 飞行器设计与工程, 学士

三、工作经历

(1) 2021-07 至 今, 南京航空航天大学，博士后/长空博士后

(2) 2024-01 至 今, 南京航空航天大学，讲师

(3) 2024-06 至 今, National University of Singapore，访问学者

四、论文

1.Zhiyuan Hu, Yang Liu, Yongjie Shi, Guohua Xu. An experimental study on rotor aerodynamic noise control based on active flap control[J]. Aerospace, 2023, 10(2): 121.

2.Zhiyuan Hu, Guohua Xu, Yongjie Shi, Runze Xia. Airfoil–vortex interaction noise control mechanism based on active flap control [J]. Journal of Aerospace Engineering, 2022, 35(1): 04021111.

3.Zhiyuan Hu, Guohua Xu, Yongjie Shi. A robust overset assembly method for multiple overlapping bodies. International Journal for Numerical Methods in Fluids. 2021, 93:653-682.

4.Zhiyuan Hu, Guohua Xu, Yongjie Shi. A new study on the gap effect of an airfoil with active flap control based on the overset grid method. International Journal of Aeronautical and Space Sciences, 2021, 22: 779-801.

5.Zhiyuan Hu, Runze Xia, Yongjie Shi, Guohua Xu. Numerical study on aerodynamic and noise responses of rotor with ramp increase in collective pitch based on time-accurate free-wake method[J]. Machines. 2023; 11(11):1007.

6.Zhiyuan Hu, Peng Yu, Guohua Xu, Yongjie Shi. Comparative Study of Soft in-Plane and Stiff in-Plane Tiltrotor Blade Aerodynamics in Conversion Flight Using CFD-CSD Coupling Approach. Aerospace. 2024; 11(1):77.

7.Peng Yu, Zhiyuan Hu, Jiaxun Hu, Guohua Xu, Yongjie Shi. Numerical studies on the aeroelasticity of a shipboard helicopter rotor during engagement and disengagement with ship motions using CFD/CSD coupling approach[J]. Aerospace Science and Technology, 2023, : 108559. (通信作者)

8.Runze Xia, Zhiyuan Hu, Yongjie Shi, Guohua Xu. Parameter analysis of active flap control for rotor aerodynamic control and design [J]. International Journal of Aerospace Engineering, 2023. (通信作者)

9.刘琦，史勇杰，胡志远，徐国华．共轴刚性旋翼气动及噪声特性的参数影响分析[J]．航空学报, 2023, 40(X) (通信作者)

五、主要专利&软著

1.胡志远，史勇杰，徐国华，孙岩，夏润泽，马太行. 一种主动控制旋翼的数值分析方法及系统. ZL202110496238.8

2.胡志远，史勇杰，徐国华，刘洋，朱嘉豪. 一种基于图形处理器的直升机流场数值模拟系统及方法. ZL202210516285.9

3.胡志远，史勇杰，徐国华，杨玉成，陆思佳. 一种CFD并行计算方法. ZL201910054745.9

4.胡志远，史勇杰，杨玉成，徐国华. 一种复杂运动的运动描述建模方法及系统. ZL201910187086.6

5.Hu Zhiyuan，Shi Yongjie，Xu Guohua，Liu Yang，Zhu Jiahao. Numerical Simulation System and Method for Helicopter Flow Field Based on Graphics Processor. PCT/CN2023/091413

6.旋翼气动与噪声综合分析软件. 2024SR0667753

7.可变形旋翼气动噪声预估软件. 2024SR0971792

8.基于源时间法的旋翼气动噪声计算软件. 2024SR0668042