Professor
Phone: +86 15829547519
Email: 2019010184@hust.edu.cn
Academic Areas: Aerodynamics and Aeroacoustics
Research Interests: Flow, Vibration and Noise Control
Academic Degrees
PhD in Power Engineering and Engineering Thermophysics, 2010, Xi’an Jiaotong University
Professional Experience
2019.07-Present, Professor, School of Aerospace, Huazhong University of Science and Technology;
2017.04-2019.03, Research Fellow, Rolls-Royce University Technology Centre in Gas Turbine Noise, University of Southampton;
2015.08-2016.07, Visiting Scholar, Aerodynamics and Flight Mechanics Group, University of Southampton;
2014.01-2019.06, Associate Professor, School of Energy and Power Engineering, Xian Jiaotong University;
2011.03-2013.12, Lecturer, School of Energy and Power Engineering, Xi’an Jiaotong University;
2009.07-2010.12, PhD Student, School of Energy and Power Engineering, Xi’an Jiaotong University;
2006.04-2007.07, Assistant Engineer, CISDI Engineering Co., Ltd;
2003.09-2006.03, Graduate Student, School of Energy and Power Engineering, Xi’an Jiaotong University;
1999.09-2003.09, Undergraduate Student, School of Energy and Power Engineering & School of Law, Huazhong University of Science and Technology
Selected Publications
Journal Papers:
[1] Xu Chen, Mao Yijun*, Hu Zhiwei. Improved equivalent source method to predict sound scattered by solid surfaces. AIAA Journal. 2019, 57(2): 513-520.
[2] Xu Chen*, Mao Yijun, Hu Zhiwei. Control of cylinder wake flow and noise through a downstream porous treatment. Aerospace Science and Technology. 2019, 88: 233-243.
[3] Xu Chen, Mao Yijun*, Hu Zhiwei. Numerical study of pore-scale flow and noise of an open cell metal foam. Aerospace Science and Technology. 2018. 82:185-198.
[4] Mao Yijun*, Hu Zhiwei, Xu Chen, Ghorbaniasl Ghader. Vector aeroacoustics for a uniform mean flow: acoustic velocity and vortical velocity. AIAA Journal. 2018, 56(7): 2782-2793.
[5] Xu Chen, Mao Yijun*, Hu Zhiwei, Ghorbaniasl Ghader. Vector aeroacoustics for a uniform mean flow: acoustic intensity and acoustic power. AIAA Journal. 2018, 56(7): 2794-2805.
[6] Mao Yijun*, Hu Zhiwei. Acoustic analogy for multiphase or multicomponent flow. ASME Journal of Vibration and Acoustics. 2018: 140(2): 021006.
[7] Zhang Qunlin, Mao Yijun*, Qi Datong. Analytical modelling of the vibro-acoustic response of a double-walled cylindrical shell with micro-perforation excited by turbulent boundary layer pressure fluctuations. ASME Journal of Vibration and Acoustics.2018, 140(2): 021012.
[8] Zhou Huihui, Mao Yijun*, Zhang Qunlin, Zhao Cun, Qi Datong, Diao Quan. Vibro-acoustics of a pipeline centrifugal Compressor, Part I, experimental study. Applied Acoustics. 2018, 131:112-128.
[9] Zhang Qunlin, Mao Yijun*, Zhou Huihui. Vibro-acoustics of a pipeline centrifugal Compressor, Part II, control with the micro-perforated panel. Applied Acoustics. 2018, 132: 152-166.
[10] Mao Yijun*, Hu Zhiwei, Gu Yuanyuan. Efficient method to predict rotor noise scattered by an axisymmetric body. AIAA Journal. 2017, 55(10): 3458-3466.
[11] Xu Chen, Mao Yijun*, Hu Zhiwei. Tonal and broadband noise control of an axial flow fan with metal foams: design and experimental validation. Applied Acoustics. 2017, 127:346-353.
[12] Zhang Qunlin, Mao Yijun*, Qi Datong. Effect of perforation on the sound transmission through a double-walled cylindrical shell. Jounal of Sound and Vibration. 2017, 410: 344-363.
[13] Mao Yijun*, Tang Hongtao, Xu Chen. Vector wave equation of aeroacoustics and acoustic velocity formulations for quadrupole source. AIAA Journal. 2016, 54(6):1922-1931.
[14] Mao Yijun*, Gu Yuanyuan, Xu Chen. Validation of frequency-domain method to compute noise radiated from rotating source and scattered by surface. AIAA Journal. 2016, 54(4): 1188-1197.
[15] Mao Yijun*, Xu Chen. Accelerated method for predicting acoustic far field and acoustic power of rotating source. AIAA Journal. 2016, 54(2): 603-615.
[16] Mao Yijun*, Xu Chen. Analytical acoustic power spectrum formulations for rotating monopole and dipole point sources. ASME Journal of Vibration and Acoustics. 2016, 138(2): 021009.
[17] Xu Chen, Mao Yijun*. Passive control of centrifugal fan noise by employing open-cell metal foam. Applied Acoustics. 2016, 103: 10-19.
[18] Xu Chen, Mao Yijun*. Experimental investigation of metal foam for controlling centrifugal fan noise. Applied Acoustics. 2016, 104: 182-192.
[19] Wen Xuanfeng, Mao Yijun*, Yang Xin, Qi Datong. Design method of the volute profile of a squirrel cage fan with space limitation. ASME Journal of Turbomachinery. 2016, 138(8): 081001.
[20] Mao Yijun*, Cai Jiancheng, Gu Yuanyuan, Qi Datong. Direct evaluation of acoustic intensity vector field around impedance scattering body. AIAA Journal. 2015, 53(5): 1362-1371.
[21] Mao Yijun*, Zhang Qunlin, Xu Chen, Qi Datong. Two types of frequency-domain acoustic-velocity formulations for rotating thickness and loading sources. AIAA Journal. 2015, 53(3): 713-722.
[22] Mao Yijun*, Xu Chen, Qi Datong. Computation of instantaneous and time-averaged active acoustic intensity field around rotating source. Journal of Sound and Vibration. 2015, 337: 95-115.
[23] Maoyijun*, Xu Chen, Qi Datong. Analytical solution for sound radiated from the rotating point source in uniform subsonic axial flow. Applied Acoustics. 2015, 92(5): 6-11.
[24] Zhang Qunlin, Mao Yijun*, Qi Datong, Gu Yuanyuan. An improved series expansion method to accelerate the multi-frequency acoustic radiation prediction. Journal of Computational Acoustics. 2015, 23(1): 1450015.
[25] Xu Chen, Mao Yijun*, Qi Datong. Frequency-domain acoustic pressure formulation for rotating source in uniform subsonic inflow with arbitrary direction. Journal of Sound and Vibration. 2014, 333(14): 3081-3091.
[26] Mao Yijun*, Xu Chen, Qi Datong, Tang Hongtao. Series expansion solution for sound radiation from rotating quadrupole point source. AIAA Journal. 2014,52(5): 1086-1095.
[27] Mao Yijun, Xu Chen, Qi Datong*. Frequency-domain model of tonal blade thickness and loading noise. Journal of the Acoustical Society of America. 2014,135(1): 93-103. [Erratum,2015, 137(4):2180]
[28] Tang Hongtao, Qi Datong, Mao Yijun*. Analysis on the frequency-domain numerical method to compute the noise radiated from rotating sources. Journal of Sound and Vibration.2013.332(23): 6093-6103.
[29] Tang Hongtao, Mao Yijun*, Qi Datong. Solution Characteristics of the Retarded-Time Equation for Transonic Rotating Sources. AIAA Journal 2013, 51(8): 2035-2040.
[30] Mao Yijun, Gu Yuanyuan, Qi Datong*. An exact frequency-domain solution of the sound radiated from the rotating dipole point source. Journal of the Acoustical Society of America.2012.132(3): 1294-1302.
Book:
[31] Qi Datong，Li Jinyin，Wen Suping，Qin Guoliang，Mao Yijun. Principal of Centrifugal Compressor (In Chinese). China Machinery Industry Press, 2018.
Courses Taught
Principle of Turbomachinery
Fundamental of Aeroacoustics and Noise Control Technique
Projects
National Natural Science Foundation of China (2015-2018): Vector Aeroacoustics Method for Rotating Blades.
International Exchange Scheme Funded by National Natural Science Foundation of China and Newton Fund of United Kingdom (2015-2017): High-Fidelity Simulations and Modelling of Wall Pressure on Blade Surfaces
National Natural Science Foundation of China (2013-2015): Noise Mechanism and Control Method for Non-compact Impedance Blade.
Natural Science Foundation of Shaanxi Province (2014-2016): Design Method of Radial Inlet Chamber of Centrifugal Compressor.
Doctoral Program of Higher Education of China(2013-2015): Efficient Noise Prediction Method for Rotating Sources
Awards
Award of Production-Study-Research Cooperation in Noise Control of Gas Turbo Compressor, Issued by China Industry-University-Research Institute Collaboration Association, 1st Prize, 2015.
