【人物简介】

　　许和勇，男，1980年12月生于安徽省肥东县，西北工业大学航空学院副教授，硕士生导师。本科毕业于西北工业大学原飞机系飞行器设计与工程专业，分别于2006年、2009年获得西北工业大学航空学院流体力学硕士、博士学位，随后进入航空宇航科学与技术博士后流动站从事与航空航天密切相关的博士后研究，2011年7月博士后出站留校任教。

【研究方向】

理论与计算流体力学、非结构网格技术、复杂流动数值模拟技术。

【研究成果】

授权专利6项： [1] 许和勇，邢世龙，杨慧强，乔晨亮，叶正寅. 一种涵道风扇唇口充气气囊及其流动分离控制方法，ZL201610422444.3，2018. [2] 许和勇，邢世龙，叶正寅. 一种直升机旋翼动态失速主动流动控制装置及方法，ZL201610363864.9 , 2018. [3] 许和勇，杨慧强，乔晨亮，邢世龙，叶正寅. 用于直升机旋翼叶片的联合射流控制装置及其控制方法， ZL201610624036.6 , 2018. [4] 许和勇，乔晨亮，杨慧强，邢世龙，叶正寅. 一种钝后缘风力机翼型环量控制装置， ZL201620737315.9, 2016. [5] 许和勇，董庆利，巩文秀，叶正寅. 基于整流罩和Coanda射流效应的汽车尾部减阻装置， ZL201621098993.1，2017. [6] 许和勇，杨慧强，叶正寅. 基于联合射流技术的风力机叶片流动控制装置， ZL201621453047.4，2017. 计算机软件著作权2项： [1]第一完成人，“基于非结构旋转嵌套网格的非定常流动数值模拟软件V1.0”，编号：2016SR195463，2016. [2]第一完成人，“基于约束Delaunay方法的非结构混合网格生成软件V1.0”，编号：2016SR195576，2016.

【科研项目】

　　主持部级预研基金1项、博士后科学基金面上项目1项、西北工业大学基础研究基金1项，参与包括重大基础技术研究项目、国家自然科学基金在内的纵横向项目10余项。

【论文著作】

发表论文共30余篇，其中第一作者SCI期刊论文 13 篇，EI索引近30篇。 英文论文发表： [1] Xu He-Yong*,Dong Qing-Li, Qiao Chen-Liang, Ye Zheng-Yin. Flow Control over the Blunt Trailing Edge Wind Turbine Airfoil Using Circulation Control. Energies, 2018, 11(3): 619. （SCI源刊） [2] Xu He-Yong*, Qiao Chen-Liang, Yang Hui-Qiang, Ye Zheng-Yin. Active Circulation Control on the Blunt Trailing Edge Wind Turbine Airfoil. AIAA Journal, 2018, 56(2): 554-570. （SCI：000423512500010，EI：20180604759693） [3] Xu He-Yong*, Yang Hui-Qiang, Ye Zheng-Yin, Zhang Dong. Numerical Study of the Discrete Staggered Staged Sonic Jet Interaction in a Supersonic Crossflow. AIAA Paper 2017-2147. 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China. (EI: 20171603581668) [4] Xu He-Yong*, Qiao Chen-Liang, Yang Hui-Qiang, Ye Zheng-Yin. Delayed Detached Eddy Simulation of the Wind Turbine Airfoil S809 for Angles of Attack up to 90 Degrees. Energy, 2017, 118: 1090-1109. （SCI：000395048900093 , EI: 20165103151354） (五年平均IF=5.18，工程技术1区top期刊) [5] Xu He-Yong*, Xing Shi-Long, Ye Zheng-Yin, Ma Ming-Sheng. A simple and conservative unstructured sliding-mesh approach for rotor-fuselage aerodynamic interaction simulation. Proceedings of the institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 2017, 231(1): 163-179. （SCI: 000397214800012 , EI: 20165203161068） [6] Xu He-Yong*, Qiao Chen-Liang, Ye Zheng-Yin. Dynamic Stall Control on the Wind Turbine Airfoil via a Co-Flow Jet. Energies, 2016, 9(6), 429:1-25. (SCI：000378854400042) [7] Xu He-yong*, Xing Shi-long, Ye Zheng-yin. Numerical Study of an Airfoil/Rotating-Slotted-Cylinder Based Flutter Exciter, Journal of Aircraft, 2015,52(6):2100-2105. （SCI: 000366158700030, EI: 20155101682400 ） [8] Xu He-yong*, Xing Shi-long, Ye Zheng-yin. Investigation on the Unstructured Rotational Dynamic Overset Grids, Aircraft Engineering and Aerospace Technology, 2015, 87(4): 293-304. (SCI：000357385900001，EI: 20153001060589) [9] Xu He-yong*, Xing Shi-long, Ye Zheng-yin. Numerical Study of the S809 Airfoil Aerodynamic Performance Using a Co-Flow Jet Active Control Concept, Journal of Renewable and Sustainable Energy, 2015, 7(2), 023131, pp: 1-20. (SCI：000353834300031，EI: 20151800802363) [10] Xu He-yong*, Xing Shi-long, Ye Zheng-yin. Numerical study of ducted-fan lip stall suppression based on inflatable leading lip cell, Procedia Engineering, 2015, 126: 158-162.(7th International Conference on Fluid Mechanics, ICFM7, 24-27 May, Qingdao, 2015) （EI: 20162302457477） [11] Xu He-yong*, Xing Shi-long, Ye Zheng-yin. Numerical simulation of the effect of a co-flow jet on the wind turbine airfoil aerodynamic characteristics,Procedia Engineering, 2015, 126: 706-710. (7th International Conference on Fluid Mechanics, ICFM7, 24-27 May, Qingdao, 2015) （EI: 20162302457382） [12] Yang Yun-chao*, Xu He-yong, Wang Jian-lei, Zha Ge-cheng. Large eddy simulation of base drag reduction with jet boat-tail passive flow control,Procedia Engineering, 2015, 126: 150-157.(7th International Conference on Fluid Mechanics, ICFM7, 24-27 May, Qingdao, 2015) （EI: 20162302457522） [13] Xu He-yong*, Ye Zheng-yin. Numerical Simulation of Rotor-Airframe Aerodynamic Interaction based on Unstructured Dynamic Overset Grids, Science China Technological Sciences, 2012, 55(10): 2798-2807. (SCI：000308701800014，EI: 20124915756581) [14] Xu He-yong*, Ye Zheng-yin. Numerical Study of Propeller Slipstream based on Unstructured Dynamic Overset Grids, Journal of Aircraft, 2012, 49(2): 384-389. (SCI:000302758400004,EI: 20121514934831) [15] Xu He-yong*, Ye Zheng-yin. Euler Calculation of Rotor-Airframe Interaction Based on Unstructured Overset Grids, Journal of Aircraft, 2011, 48(2): 707-712. (SCI: 000289705400036，EI: 20111413897708) [16] Xu He-yong*, Ye Zheng-yin. Numerical Simulation of Unsteady Flow around Forward Flight Helicopter with Coaxial Rotors, Chinese Journal of Aeronautics, 2011, 24(1): 1-7. (SCI: 000290753200001，EI: 20111113740590) [17] Xu He-yong, Ye Zheng-yin. Investigation of a flutter exciter for aircraft flight testing using unstructured overset grids. AIAA Paper 2011-6670. AIAA Atmospheric Flight Mechanics Conference, 08-11 August 2011, Portland, Oregon, USA. (EI: 20133616685066) [18] Xu He-yong, Ye Zheng-yin. Numerical simulation of rotor-airframe aerodynamics using technology of unstructured overset grids. AIAA Paper 2011-6724. AIAA Modeling and Simulation Technologies Conference, 08-11 August 2011, Portland, Oregon, USA. (EI: 20133116554696) [19] Xu He-yong *, Ye Zheng-yin. Coaxial Rotor Helicopter in Hover Based on Unstructured Dynamic Overset Grids, Journal of Aircraft, 2010, 47(5):1820-1824. (SCI: 000283206100037，EI: 20104513358547) [20] Xu He-yong, Ye Zheng-yin, Wang Gang, Shi Ai-ming. Numerical Simulation of Unsteady Rotor-Fuselage Aerodynamic Interaction, Acta Aerodynamic Sinica(空气动力学学报英文)，2010，28(2): 162-167. (EI: 20102212966460) [21] Xu He-yong, Ye Zheng-yin, Wang Gang, Shi Ai-ming. Simulation of Helicopter Forward Flight Flow Using Unstructured Overset Grids. AIAA Paper 2009-1285, 2009. （EI: 20104713414702） [22] Xu He-yong, Ye Zheng-yin, Wang Gang. Unstructured Dynamic Patched Grid Method and Application. Proceedings of the Sino-Russian Conference on Aerospace Technology. 2006，Northwestern Polytechnical University, China, pp:291～296 (ISBN: 7-5612-2079-0/TH235) 中文论文发表（2011年以来）： [1] 许和勇，邢世龙，叶正寅，马明生. 基于充气前缘技术的旋翼翼型动态失速抑制研究，航空学报，2017，38（6）：120799 （EI: 20173804185284） [2] 苏运德，叶正寅，许和勇. 桨尖间隙和双桨间距对涵道螺旋桨气动性能的影响，航空动力学报 ，2014，29(6):1468-1475. （EI: 20142817936114） [3] 许和勇，叶正寅. 基于非结构嵌套网格的涵道螺旋桨数值模拟，空气动力学学报，2013, 31(3): 306-309. [4] 陈杰，马存宝，许和勇. 野战环境下大型飞机超低空气动特性分析，飞行力学 ，2013,31(3):217-220,229. [5] 许和勇，叶正寅，张伟伟. 基于非结构自适应网格技术的高超声速流动数值模拟，工程力学，2012,29(3):226-229. (EI: 20121514940741) [6] 许和勇，叶正寅. 涵道螺旋桨与孤立螺旋桨气动特性的数值模拟对比，航空动力学报，2011，26(12): 2820-2825. (EI: 20120314703007) [7] 许和勇，叶正寅. 三维非结构自适应多重网格技术，空气动力学学报，2011，29(3): 229-233. (EI: 20113014176604) [8] 许和勇，叶正寅. 非结构旋转动态嵌套网格技术及其应用，西北工业大学学报，2011，29(2): 171-175. ( EI: 20112214022679)