胡峪

综合介绍 General Introduction 主要研究方向：    飞机总体设计    飞机外形优化设计    新概念无人机（复合固定翼、倾转旋翼、涵道飞行器、滚翼机等）    虚拟现实/增强现实技术在飞行器模拟仿真中的应用 个人相册

教育教学

个人经历 personal experience 工作经历 1992-1996，西北工业大学飞机设计专业学士学位 1995-1998，西北工业大学飞机设计专业硕士学位 1998-2001，西北工业大学飞机设计专业博士学位 2001-2003，清华大学精密仪器系博士后 2003-2007，新加坡国立大学Research fellow 2007-2009，新加坡微软程序员 2009-现在，西北工业大学航空学院副教授（2009）

荣誉获奖

学科信息 Subject information

科学研究

教育教学 Education and teaching 招生信息 教育信息 研究方向：1、飞行器总体设计2、飞行器外形设计优化3、新概念无人飞行器 学生就业及毕业情况：     主要集中于航空航天和兵器工业主机所，其中有航天1院、中航技、中航工业603、618所、626所、上海商飞、核工业部9院（绵阳）和兵器工业部203所等。     获得优秀硕士毕业生称号4人次，获得国家奖学金2人次，获得西北工业大学学术达人1人次  1、飞机总体设计，本科生课程， 56学时 2、航空概论，国际班课程， 24学时

学术成果

科研成果 Scientific research results 论文成果 专利成果 软件著作权 专著成果 其他成果 [1] 摆线桨非定常气动特性研究.航空学报,2014,35(07) [2] 利用螺旋桨动力配平的飞翼布局无人机.西北工业大学学报,2014,32(02) [3] The effect of aerofoil camber on cycloidal propellers.AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,8 [4] The effects of dynamic-stall and parallel BVI on cycloidal rotor.AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY,1 [5] An unsteady free wake model for aerodynamic performance of cycloidal propellers.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,2 [6] Optimal design and endurance estimation of propulsion system for electric-powered unmanned aerial vehicle.Hangkong Dongli Xuebao/Journal of Aerospace Power,8 [7] Tailless UAV design optimization under center of gravity location uncertainty.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,7 [8] Optimum Design for Hand-launched Flying Wing Mini-UAV Based on the Cambered Airfoil.DISCOVERY, INNOVATION AND COMMUNICATION - 5TH CSAA SCIENCE AND TECHNIQUE YOUTH FORUM, [9] Investigation on the unsteady aerodynamics of cycloidal propeller in hovering flight.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING,13 [10] A novel coherent column replacement method in compressed sensing for DOA estimation.Chinese Control Conference, CCC, [11] Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude.Chinese Journal of Aeronautics,5 [12] 基于正弯度翼型的手掷飞翼布局小型无人机优化设计.探索 创新 交流——第五届中国航空学会青年科技论坛,中国江西南昌 [13] A detailed aerodynamic analysis of the cyclorotor using dynamic mesh in CFD.52nd Aerospace Sciences Meeting, [14] The effects of blade aspect ratio and taper ratio on the hovering performance of the cycloidal rotor.35th AIAA Applied Aerodynamics Conference, 2017, [15] Compressed sensing based joint detection and tracking for STAP radar.FUSION 2016 - 19th International Conference on Information Fusion, Proceedings, [16] Two dimensional numerical simulation of cycloidal propellers with flat plate airfoil in hovering status.2013 International Powered Lift Conference, [17] A novel compressed sensing based method for reconstructing sparse signal using space-time data in airborne radar system.Chinese Control Conference, CCC, [18] Robust design consideration in the multi-disciplinary optimization of a flying wing UAV design.52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, [19] The multi-disciplinary robust optimization for tailless aircraft.AIAA AVIATION 2014 -15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, [20] The multi-disciplinary optimization for aircraft design based on self-adaptive approximation model.AIAA AVIATION 2014 -14th AIAA Aviation Technology, Integration, and Operations Conference, [21] Hovering efficiency optimization of the ducted propeller with weight penalty taken into account.AEROSPACE SCIENCE AND TECHNOLOGY, [22] Unsteady Aerodynamic Optimization of Airfoil for Cycloidal Propellers Based on Surrogate Model.JOURNAL OF AIRCRAFT,4 [23] A flying wing UAV trimmed with propeller thrust.Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University,2 [24] Research on the unsteady aerodynamic characteristics of cycloidal propeller.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,7 [25] 滚翼机滚转阶跃响应分析.飞行力学,2014,32(02) [26] 电动飞翼布局无人机设计研究.飞行力学,2013,31(01) [27] 摆线桨气动性能研究进展.空气动力学学报,2013,31(05) [28] 基于LB动态失速模型的摆线桨气动性能计算方法.飞行力学,2011,29(03) [29] 考虑重心位置不确定性的无尾无人机优化设计.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,

综合介绍

获奖信息 The winning information 1、2018.8，   研究生创新飞行器大赛全国一等奖2、2013.9，“风火轮”滚翼机II，2013年度国际微小型无人机大赛（IMAV2013）一等奖3、2011.9，“风火轮”滚翼机，中航工业杯无人机创新大奖赛国际二等奖