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更新日期：2024年3月27日 姓 名 杨延年 性 别 男 出生年月 1985年7月 籍贯 湖北荆州市 民 族 汉族 政治面貌 最后学历 博士研究生 最后学位 工学博士 技术职称 副教授 导师类别 博、硕导 行政职务 Email yangyn@scut.edu.cn 工作单位 华南理工大学 邮政编码 510641 通讯地址 广州市天河区五山路381号华南理工大学3号楼501室 单位电话 87113401 个人主页 http://www2.scut.edu.cn/automation/ 个人简介 本硕毕业于西北工业大学航空学院，博士毕业于荷兰代尔夫特理工大学航空宇航学院。主要从事无人机旋翼优化设计、图像处理、风洞测试、旋翼气动建模、空气动力学、气动声学。以第一作者在Jounal of Fluid Mechanics、Physics of Fluids、AIAA Journal、Journal of Sound and Vibration等领域类顶级期刊上发表了一系列研究成果。主持过国家、省、市级项目7项。曾获全国航空航天模型锦标赛3公斤限时载运空投冠军，Physics of Fluids文章被选为Editor's pick以及featured article 。担任AIAA Journal、Physics of Fluids、实验流体力学等国内外期刊审稿人。 工作经历 2016.07-2017.08   工程师，亿航智能设备有限公司，广州2017.09-2022.6    研究助理教授, 南方科技大学力学与航空航天工程系，深圳 2022.6-今        副教授，华南理工大学自动化科学与工程学院，广州Work experience2016.7- 2017.8 Job title: Engineer；Company: eHANG2017.9- 2022.6 Job title: Research assistant professor；Institute: Southern University of Science and Technology2022.6-Now Job title: Associate professor; Institute: Soutch China University of Technology 教育经历 2011.10-2017.3    博士，空气动力学，航空宇航学院，代尔夫特理工大学，荷兰2009.09-2011.09   硕士，飞行器设计，航空学院，西北工业大学, 陕西省西安市2005.09-2009.06   本科, 飞行器设计与工程，航空学院，西北工业大学, 陕西省西安市Education history2005.9-2009.7 Bachelor, Aircraft design and engineering, School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi Province, China2009.9-2011.9 Master, Aircraft design, School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi Province, China2011.10-2017.3 PhD, Department of aerodynamics, wind energy, and flight performance and propulsion, Faculty of Aerospace Engineering, Delft University of Technology, Netherlands. Supervisors: Georg Eitelberg and Leo Veldhuis. 获奖、荣誉称号 2008年中国航空航天模型锦标赛团体第一名，飞行组第二名第15届挑战杯广东省大学生课外学术科技作品竞赛二、三等奖各一项，第一指导老师深圳市海外高层次人才孔雀计划C类HonorsNational champion of aero modeling completion of ‘3 kilogram weight aircraft for cargo airdrop’The 15th Challenge-cup Extracurricular and Academic Contest, Second and third prize, Prime supervisor. Recipient of the Overseas High-Calibre Personnel of Shenzhen (Peacock Program), Shenzhen 社会、学会及学术兼职 AIAA member 研究领域 无人机设计、图像处理、气动优化、螺旋桨设计、空气动力学、气动声学、机器学习、风洞设计与试验、粒子图像测速、计算流体力学Research areaUAV design, Image processing, aerodynamic optimization, propeller design, aerodynamics, aeroacoustics, machine learning, wind tunnel design and tests, PIV, CFD 科研项目 2023.11-2024.11, 环形旋翼优化设计及其在对转旋翼中的应用，中国空气动力研究与发展中心，旋翼空气动力学重点实验室,主持2022.1-2022.12 ，针对垂直起降飞行器的螺旋桨气动-声学一体化设计研究，中航通飞研究院“揭榜挂帅”技术攻关项目，主持2019.01-2021.12，中低雷诺数翼型失速流动特征及气动噪声机理研究，国家自然科学基金青年基金项目，主持2018.05-2021.04 ，垂直涡流入射对桨叶气动噪声影响及流动控制研究，广东省自然科学基金，主持2021.04-2023.04，基于仿生学的无人机旋翼降噪方法研究，深圳市优秀科技创新人才培养项目-博士启动项目，深圳市科技创新委员会，主持。2019.01-2019.12，城市区域飞行器概念研究，中国商飞北研中心，主持2019.08-2020.08，基于仿生学的旋翼尾缘锯齿降噪机理研究，中国空气动力研究与发展中心，气动噪声控制重点实验室，主持。2018.01-2020.12 ，小型无人机气动噪声机理与抑制方法研究，深圳市科创委学科布局项目，主研（排名2/8）Projects2019.01-2021.12 Aerodynamic and aeroacoustic investigation of airfoil stall，NSFC-Young Scholar，PI2018.05-2021.04 Noise emission of blade vortex interaction，NSF of Guangdong Province，PI2021.04-2023.04 Noise reduction of UAV rotors by bionic methods，PhD start-up funding，the Science and Technology Innovation Commission of Shenzhen，PI2022.1-2022.12 Aerodynamics and aeroacoustic design of electric Vertical Take off and landing (eVTOL) flight vehicle propellers，China Aviation Industry General Aircraft Co. Ltd.，PI 2019.01-2019.12 Design of urban air mobility vehicles，COMAC Beijing，50,000，No. B2019JS32020, PI2019.08-2020.08 Noise reduction of UAV rotors by trailing edge serrations, CARDC，PI。2018.01-2020.12 Noise generation mechanism and mitigation methods for small UAVs，the Science and Technology Innovation Commission of Shenzhen, Participate 发表论文 期刊论文，Journal articles[29] Yang, Y.; Liang, Y.; Pröbsting, S.; Li, P.; Zhang, H.; Huang, B.; Liu, C.; Pei, H.; Noack, B.R. Sizing of Multicopter Air Taxis—Weight, Endurance, and Range. Aerospace 2024, 11, 200.[28] Pengyu Li, Yannian Yang, Qingxi Li, Elias J. G. Arcondoulis, Bernd R. Noack, Yu Liu; Effect of blade number on rotor efficiency and noise emission at hovering condition. Physics of Fluids 1 February 2024; 36 (2): 027142. (JCR一区)[27] Yang Yannian, Li Chenzhao, Pröbsting Stefan, Liu Xiaomin, Liu Yu, Arcondoulis J.G. Elias, Hysteresis effect on airfoil stall noise and flow field, Phys. Fluids 35(9):095101, 2023). (JCR一区)[26] Wang Tianyu, Yang Yannian, Chen Xuanwu, Li Pengyu, Iollo Angelo, Maceda Guy Y. Cornejo, and Noack Bernd R., Topologically assisted optimization for rotor design，Phys. Fluids 35, 055105 ,2023). (JCR一区， 共同通讯)[25] Yang Chenghao, Arcondoulis Elias J. G., Yang Yannian, Guo Jing, Maryami Reza, Bi Chuanxing, and Liu Yu, Active control of airfoil turbulent boundary layer noisewith trailing-edge blowing, J. Acoust. Soc. Am. 153 (4), April 2023[24] Li Shoutu, Chen Qin , Li Ye, Pröbsting Stefan, Yang Congxin, Zheng Xiaobo, Yang Yannian, Zhu Weijun, Shen Wenzhong, Wu Faming, Li Deshun, Wang Tongguang, Ke Shitang, “Experimental investigation on noise characteristics of small scale vertical axis wind turbines in urban environments,” Renewable Energy, 2022 [23] Pröbsting S., Yang Y., Zhang, H., Li P., Liu Y., Li Y., “Effect of Mach number on the aeroacoustic feedback loop generating airfoil tonal noise,” Physics of Fluids, 2022. (被期刊选为Featured article) (JCR一区,Accepted,共同通讯)[22] Yang Y., Pröbsting S., Li P., Liu Y., Li Y., “A secondary modulation mechanism in aerofoil tonal self-noise generation,” Journal of Fluid Mechanics, 2022, Vol . 943, A13. (JCR一区)[21] Liang, Y., Yang, Y., Shan, X., Wang Z., “Effect of Airfoil Dimple on Low-Reynolds-Number Differing Laminar Separation Behavior via Multi-Objective Optimization,” Journal of Aircraft, 2022.                        [20] Arcondoulis, E., Liu, Y., Xu, P., Li, Q., Wei, R. Yang, Y., and Chen, N., “An experimentally based CLEAN-SC array pairing method for distributed aeroacoustic sources,” AIAA Journal (Technical Note), 2021. [19] Qian Liu， Yu Liu， Hanbo Jiang，Yannian Yang， Peng Zhou， Acoustic scattering by a finite plate with a poroelastic extension using the unified transform method， Journal of Sound and Vibration, 116677， 2021 (JCR一区)[18] Honglei Bai, Zhenbo Lu, Renke Wei, Yannian Yang, Yu Liu, “Noise reduction of sinusoidal wavy cylinder in subcritical flow regime,” Physics of Fluids, Vol.33，105120，2021. (JCR一区)[17] Yannian Yang, S. Pröbsting, Y. Liu, H. Zhang, C. Li, and Y. Li, “Effect of dual vortex shedding on airfoil tonal noise generation,” Physics of Fluids, Vol.33，075102，2021. (JCR一区)[16] Haitao Hu, Yannian Yang, Yu liu, Xiaomin Liu, Yong Wang, “Aerodynamic and aeroacoustic investigations of multi-copter rotors with leading edge serrations during forward flight,” Aerospace Science and Technology, Vol. 112,, 106669, 2021. (JCR一区，共同一作)[15] Yannian Yang, Yu Liu, Rui Liu, Chao Shen, Pikai Zhang, Renke Wei, Xiaomin Liu, Pengwei Xu, “Design, validation, and benchmark tests of the aeroacoustic wind tunnel in SUSTech” Applied Acoustics, Vol. 175, 107847, 2021. [14] Yannian Yang, Yong Wang, Yu Liu, Haitao Hu, Zhiyong Li, “Noise reduction and aerodynamics of isolated multi-copter rotors with serrated trailing edges during forward flight” Journal of Sound and Vibration, Vol.489, 115688, 2020. (JCR一区)[13] Zhang P., Liu Y., Li Z, H. Liu, Yang Y., “Numerical study on reducing aerodynamic drag and noise of circular cylinders with non-uniform porous coatings,” Aerospace Science and Technology  108:106308, 2020. (JCR一区)[12] Li Z, Tang T., Liu Y., Arcondoulis, E., Yang Y., “Numerical study of aerodynamic and aeroacoustic characteristics of flow over porous coated cylinders: Effects of porous properties,” Aerospace Science and Technology 105:106042,2020. (JCR一区)[11] Yang, Y., Liu, Y., Li, Y., Arcondoulis, E., Wang Y., “Aerodynamic and Aeroacoustic Performance of an Isolated Multicopter Rotor During Forward Flight,” AIAA Journal, Vol. 58 No. 3, 2020, pp. 1171-1181. （航空航天顶刊）[10] Yang Y., Liu Y., Hu H., Liu X., Wang Y., Arcondoulis E., Li Z., Experimental study on noise reduction of a wavy multi-copter rotor, Appllied Acoustics, Vol. 165, 2020, 107311. [9] Li Z, Tang T., Liu Y., Arcondoulis, E., Yang Y., Implementation of compressible porous-fluid coupling method in an aerodynamics and aeroacoustics code - Part II: Turbulent flow, Applied Mathematics and Computation 373:124988,2020(JCR一区)[8] Arcondoulis, E., Liu, Y., Li, Z., Yang, Y., Wang Y., “Structured Porous Material Design for Passive Flow and Noise Control of Cylinders in Uniform Flow,” Materials 12(18):2905, 2019[7] Yang, Y., Sciacchitano, A., Veldhuis, L., and Eitelberg, G., “Spatial-temporal and modal analysis of propeller induced ground vortices by particle image velocimetry,” Physics of Fluids, Vol. 28, 105103, 2016. (被期刊选为Editor’s Pick) (JCR一区)[6] Yang, Y., Zhou, T., Sciacchitano, A., Veldhuis, L., and Eitelberg, G., “Experimental investigation of the impact of a propeller on a streamwise impinging vortex,” Aerospace Science and Technology, Vol. 69, pp. 582-594, 2017. (JCR一区)[5] Yang, Y., Veldhuis, L., and Eitelberg, G., “Aerodynamic impact of a streamwise vortex on a propeller,” Aerospace Science and Technology, Vol. 70, pp. 108-120, 2017. (JCR一区)[4] Yang， Y., Zhou, T., Sciacchitano, A., Veldhuis, L., and Eitelberg, G., “Propeller and inflow vortex interaction: vortex response and impact on the propeller performance,” CEAS Aeronautical Journal, Vol. 7, No. 3, pp.419-428, 2016.[3] Yang, Y., Sciacchitano, A., Veldhuis, L., and Eitelberg, G., “Analysis of propeller-induced ground vortices by particle image velocimetry,” Journal of Visualization， Vol. 21, Issue 1, pp. 39-55, 2018. [2] Yang, Y., Veldhuis, L., and Eitelberg, G., “Numerical analysis of propeller induced ground vortices by actuator disk model,” Journal of Visualization， Vol. 21, Issue 1, pp. 117-132, 2018.[1] 杨延年，张元明，“一种新型无人飞行器的现状与关键技术分析”，航空工程进展，Vol. 2, No.1, 2011. 出版专著和教材 无 科研创新 [5]杨延年,一种飞行器及系统，中国实用新型专利, 201621209719.7.[4]杨延年，刘宇，单肖文，一种外缘式电力推进喷气发动机系统，中国实用新型专利，201721552212.6[3]杨延年，刘宇，单肖文，一种外缘式电力推进喷气发动机系统及设计方法，中国发明专利，201711144190.4[2] 陈炫午，杨延年，刘宇，一种旋翼飞行器，中国实用新型专利，2020020913068.X[1] 许振宇，单肖文，王浩，杨延年，张浩天，一种利用鸭翼翼尖螺旋桨加强涡增升的飞行器，CN207943171UPatents[5]Yang, Y., An unmanned aerial vehicle and system，China, 201621209719.7.[4]Yang, Y.，Liu, Y., and Shan, X.，Rim-driven electric propulsive fan system，China，201721552212.6[3] Yang, Y.，Liu, Y., and Shan, X.，Rim-driven electric propulsive fan system and design method，China，201711144190.4[2] Chen, X., Yang, Y., and Liu, Y., A rotor powered aerial vehicle，China，2020020913068.X[1] Xu, Z., Shan, X., Wang, H., Yang, Y., and Zhang, H., An aerial vehicle with propeller on the canard tip for lift augmentation，China, CN207943171U 教学活动 《信号分析与处理》本科生课程，32学时主上《飞行器设计原理》本科生课程，72学时。助教《风洞仿真》本科生课程，32学时。助教《空气动力学》，16学时Lecture experience  2022.03-2022.06  Singnal analysis and processing, SCUT, 32 cources2020.09-2020.12 Lecturer, ‘Aircraft Group Design’, SUSTech, 72 courses. 2012- 2015 Student practical guide, ‘Wind tunnel simulation’, TU Delft. 2013.3 Student practical guide, ‘Aerodynamics’, TU Delft. 指导学生情况 曾指导硕士、本科毕设课题：“无人机螺旋桨锯齿尾缘降噪技术应用与研究”、“无人机螺旋桨前缘锯齿降噪机理及设计”、“翼型大攻角失速流动特征及噪声机理研究”、“安静城市区域飞行器设计”、“旋翼优化设计方法研究”、“垂直入射涡流对翼型气动噪声特征影响及机理研究”、“基于遗传算法的城市飞行器旋翼优化设计”、“基于格子玻尔兹曼方法的城市飞行器噪声分析、”Orthogonal vortex and propeller interaction: Vortex response and propeller performance variation、“An analytical and experimental study of ground vortices”。 我的团队 招贤纳士：欢迎空气动力学、流体力学、图像处理、飞行器设计、飞行器控制领域的学生申请本团队博士后、博士、硕士