姓 名：郭昊 副教授
所在单位：空气动力学系
研究方向：气动声学、湍流、实验流体力学

联系方式：010-82339592；13511060706

通讯地址：北京市海淀区学院路37号bat365在线官网登录新主楼C601，邮编：100083
邮箱：guohao@buaa.edu.cn

详细介绍：

男，1978年12月生，博士，副教授。2001年7月在北京大学获工学学士学位，2007年3月在香港中文大学获物理学博士学位，2007年4月至2008年3月在香港中文大学物理系做博士后。现为bat365在线官网登录流体所副教授。2018年12月至2019年12月在荷兰代尔夫特理工大学从事访问学者研究。长期坚持在教学一线，先后承担过本科生必修课《空气动力学》、《航空工程大型通用软件应用》和《课程设计》，本科生选修课《粘性流体力学》、研究生选修课《飞机气动噪声控制原理及应用》和《水波动力学》的教学工作。2010年获bat365在线官网登录教学成果奖一等奖（3/5），2013年获优秀班主任，2014年指导员工获校级优秀硕士论文奖，2018年获得北京市“高等集团产品成果奖”二等奖（2/9）。科研方面，在国家自然科学基金青年基金、中欧航空科技合作项目等支持下，从事气动噪声、湍流理论及民机减阻降噪技术研究，近5年发表SCI论文约30篇。

教育背景

2001/09-2007/03，北京大学工学院&香港中文大学，流体力学，博士

1997/09-2001/07，北京大学力学与工程科学系，结构工程，学士

工作经历

2008/09-，bat365在线官网登录，流体力学，博士

2007/04-2008/03，香港中文大学，博士后

研究兴趣

气动声学与流动噪声控制：增升装置噪声、起落架噪声、钝体流动与噪声控制、腔体流动与噪声控制

气动与声学测试：流场与声场耦合测试与分析、麦克风相控阵列设计、深度学习声源成像、气动声学风洞

湍流与流动控制：转捩与湍流理论、壁面湍流与减阻控制、深度学习湍流模式

发表论文

[1 Li Ling, Liu Peiqing, Xing Yu, Guo Hao(*)，Wavelet analysis of multiple tonal phenomena generated from a simplified nose landing gear and a ring cavity，Journal of Sound and Vibration 464 (2020) 114980

[2] Li Ling, Liu Peiqing, Xing Yu, Guo Hao(*)，Shell models for confined Rayleigh-Taylor turbulent convection，Communications in Nonlinear Science & Numerical Simulation，Volume 84, May 2020, 105204

[3] Guo, Zhifei, Liu, Peiqing, Guo Hao(*). (2020). Investigation on spatial distribution of acoustic resonance in annular cavity: Frequency and intensity. International Journal of Aeroacoustics, 19(1-2), 2020, 73-94

[4] Guo, Zhifei, Liu, Peiqing, Guo Hao(*). (2020). Control effect on deep cavity noise by slanted walls at low Mach numbers, JOURNAL OF VIBRATION AND CONTROL

[5] Liu Zhenchen, Liu, Peiqing, Guo Hao(*) & Hu Tianxiang.(2020) Experimental investigations of turbulent decaying behaviors in the core-flow region of a propeller wake. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 234(2): 319-329

[6] Zhang, Wen; Liu, Peiqing; Guo, Hao(*); Qu, Qiulin; Multi-scale entropy analysis and conditional sampling of the velocity increment in a transitional boundary layer, Communications in Nonlinear Science & Numerical Simulation, Volume 67, February 2019, Pages 303-313

[7] Li Ling, Liu Peiqing, Xing Yu, Guo Hao(*)，Experimental investigation on the noise reduction method of helical cables for a circular cylinder and tandem cylinders，Applied Acoustics 152 (2019) 79-87

[8] Lu Weishuang, Liu Peiqing, Guo Hao(*)，Hu Tianxiang, Investigation on intensity of tones due to self-excited oscillation within the leading-edge slat cove at different incoming flow speeds，Applied Acoustics 155 (2019) 232–239

[9] Lu Weishuang, Liu Peiqing, Guo Hao(*)，Hu Tianxiang, Investigation on Tones due to Self-excited Oscillation within Leading-edge Slat Cove at Different Angles of Attack: Frequency and Intensity, Aerospace Science and Technology 91(2019) 59–69

[10] Li Ling, Liu Peiqing, Guo Hao(*), Geng Xin, Hou Yujia, Wang Jinjun，Aerodynamic and aeroacoustic experimental investigation of 30P30N high-lift configuration，Applied Acoustics 132 (2018) 43–48

[11] Li Ling, Liu Peiqing, Xing Yu, Guo Hao(*)，Time-frequency analysis of acoustic signals from a high-lift configuration with two wavelet functions，Applied Acoustics 129 (2018) 155–160

[12] Li Ling, Liu Peiqing, Xing Yu, Guo Hao(*)，Wavelet Analysis of the Far-Field Sound Pressure Signals Generated from a High-Lift Configuration，AIAA Journal, Vol. 56, No. 1 (2018), pp. 432-437.

[13] Zhang, Wen; Liu, Peiqing; Guo, Hao(*); Conditional sampling and wavelet analysis in the early stage of step-generated transition, AIAA Journal, Vol. 56, No. 6 (2018), pp. 2471-2477.

[14] Zhang, Wen; Liu, Peiqing; Guo, Hao(*). Correlation-Based Transition Model for Swept-Wing Flow Using the Cross-Flow Reynolds Number [J]. JOURNAL OFAIRCRAFT, Vol. 54, No. 1, 359 January–February 2017

[15] Liu, Peiqing; Xing, Yu; Guo, Hao(*); Li, Ling, Design and performance of a small-scale aeroacoustic wind tunnel, Applied Acoustics, 2017, 116: 65~69.

[16] Xing, Yu; Liu, Peiqing; Guo, Hao(*), Dual effects of buoyancy and enstrophy transfer on scaling behavior of a shell model proposed for homogeneous turbulent convection, Communications in Nonlinear Science and Numerical Simulation, 2017, 44: 74~88.

[17] Xing, Yu; Liu, Peiqing; Guo, Hao(*), Li Ling, Effect of helical cables on cylinder noise control, Applied Acoustics 122 (2017) 152–155

[18] Zhang, Wen; Liu, Peiqing; Guo, Hao(*); Wang, Jinjun Detecting the chaotic nature in a transitional boundary layer using symbolic information-theory quantifiers, PHYSICAL REVIEW E, 2017, 96:052215

[19] Li Ling, Liu Peiqing, Guo Hao(*), Hou Yujia, Geng Xin, Wang Jinjun， Aeroacoustic measurement of 30P30N high-lift configuration in the test section with Kevlar cloth and perforated plate, AEROSPACE SCIENCE AND TECHNOLOGY, 2017 70 (2017) 590–599

[20] Chen, Mingqian(*); Liu, Peiqing(*); Guo, Hao(*); Qu, Qiulin(*), Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration, Journal of Aircraft, 2016.2.JAN-FEB, 53(1): 217~230.

[21] Qin Yunpeng, Liu Peiqing, Qu Qiulin(*) and Guo Hao. Numerical study of aerodynamic forces and flow physics of a delta wing in dynamic ground effect, Aerospace Science and Technology, 2016, 51: 203-221.

[22] Qu, Qiulin(*); Wang, Rui(*); Guo, Hao(*); Liu, Peiqing(*); Agarwal, Ramesh K. (*), Numerical Study of Water Impact of an Elastic Cylindrical Shell, AIAA J, 2016, 54(10): 3295-3302

[23] Guo Hao(*); Huang, Qianmin; Liu, Peiqing; Qu, Qiulin， Effects of local high-frequency perturbation on a turbulent boundary layer by synthetic jet injection[J]. Fluid Dynamics Research, 47(4), 2015/8.

[24] Guo Hao(*); Huang, Qianmin; Liu, Peiqing; Fent Tao， Influence of localized unsteady ejection on the scaling laws and intermittency in a turbulent boundary layer flow[J]. Experiments in Fluids, 2015, 56:165

[25] Tang Zhihao，Liu Peiqing，Sun Jingwei，Chen Yaxi，Guo Hao(*)，Li Guangchao，Performance of Contra-Rotating Propellers for Stratospheric Airships，International Journal of Aeronautical and Space Sciences，2015，16（4）：485-492。

[26] Tang Zhihao，Liu Peiqing，Guo Hao(*)，Yan Jie，Li Guangchao，Two -Dimensional Moving Blade Row Interactions in a Stratospheric Airship Contra-Rotating Open Propeller Configuration，International Journal of Aeronautical and Space Sciences，2015，16（4）：500-509。

[27] Qu Qiulin(*), Lu Zhe(*), Guo Hao(*), Liu Peiqing(*) and Agarwal Ramesh K. (*). Numerical Investigation of the Aerodynamics of a Delta Wing in Ground Effect, Journal of Aircraft, 2015, 52(1): 329-340.

[28] Qu, Qiulin(*); Hu, Mingxuan(*); Guo Hao (*); Liu, Peiqing(*); Agarwal, Ramesh K. (*), Study of Ditching Characteristics of Transport Aircraft by Global Moving Mesh Method，Journal of Aircraft, 2015, 52(5): 1550-1558.

[29] Tang Zhihao，Liu Peiqing(*)，Chen Yaxi，Guo Hao，Experimental Study of Counter-Rotating Propellers for High-Altitude Airships，Journal of Propulsion and Power，2015，31（5）：1491-1496

[30] 邢宇，刘沛清(*)，郭昊，徐亮，李玲, 简化起落架噪声相似准则及马赫数比例律研究, 航空学报， 1000-6893（2016）

[31] 李玲，刘沛清(*)，邢宇，郭昊，田云，亚临界雷诺数圆柱绕流远场气动噪声实验研究，bat365在线官网登录学报，1001-5965( 2016)

[32] 王骁原，郭昊，邢宇，刘沛清(*)，LAGOON起落架缩比模型机轮空腔发声机理实验研究，航空学报，2016