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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
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
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
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
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
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
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
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
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
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
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
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.
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.
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
Liu, Peiqing; Xing, Yu; Guo, Hao(*); Li, Ling, Design and performance of a small-scale aeroacoustic wind tunnel, Applied Acoustics, 2017, 116: 65~69.
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.
Xing, Yu; Liu, Peiqing; Guo, Hao(*), Li Ling, Effect of helical cables on cylinder noise control, Applied Acoustics 122 (2017) 152–155
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
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
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.
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.
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
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.
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
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。
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。
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.
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.
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
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）
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，北京航空航天大学学报，1001-5965( 2016)
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
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