[1] 乔渭阳. 航空发动机气动声学[M]. 北京:北京航空航天大学出版社, 2010.
[2] 王良锋, 乔渭阳, 纪良, 等. 轴流风扇/压气机管道周向声模态的测量[J]. 航空动力学报, 2014, 29(4):917-926.
[3] 王良锋, 乔渭阳, 纪良, 等. 风扇进口噪声预测模型的改进[J]. 推进技术, 2015, 36(2): 226-231. (WANG Liang-feng, QIAO Wei-yang, JI Liang, et al. An Improved Prediction Model for Fan Inlet Noise[J]. Journal of Propulsion Technology, 2015, 36(2): 226-231.)
[4] 纪良, 乔渭阳, 王良锋, 等. 普通室内机翼尾缘噪声降噪的实验研究[J]. 推进技术, 2015, 36(5):703-712. (JI Liang, QIAO Wei-yang, WANG Liang-feng, et al. Experimental Investigation of Airfoil Trailing-Edge Noise Reduction in a Normal Indoor Test Bed[J]. Journal of Propulsion Technology, 2015, 36(5):703-712.)
[5] Tyler J M, Sofrin T G. Axial Flow Compressor Noise Studies[J]. Transactions of the Society of Automotive Engineers, 1962, 70: 309-332.
[6] Holste F, Neise W. Noise Source Identification in a Propfan Modal by Means of Acoustical Near Field Measurements[J]. Journal of Sound and Vibration, 1997, 203(4): 641-665.
[7] Enghardt L, Zhang Y, Neise W. Experimental Verification of a Radial Mode Analysis Technique Using Wall-Flush Mounted Sensors[C]. Berlin: 137th Meeting of the Acoustical Society of America, 1999. ?
[8] Enghardt L, Tapken U, Kornow O, et al. Acoustic Mode Decomposition of Compressor Noise under Consideration of Radial Flow Profiles[R]. AIAA 2005-2833.
[9] Faustmann C, Zerobin S, Spataro R, et al. On the Acoustics of a Turning Mid Turbine Frame with Embedded Design in a Two-Stage Test Turbine[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy, 2015, 229(5): 529-538.
[10] Arnold F, Tapken U, Bauers R, et al. Turbomachinery Exhaust Noise Radiation Experments, Part 2: In-Duct and Far-Field Mode Analysis[R]. AIAA 2008-2858.
[11] Huang X. Real-Time Location of Coherent Sound Sources by the Observer-Based Array Algorithm[J]. Measurement Science & Technology, 2011, 22(6): 065501.
[12] Castres F O, Joseph P F. Experimental Investigation of an Inversion Technique for the Determination of Broadband Duct Mode Amplitudes by Use of Near-Field Sensor Arrays[J]. Journal of the Acoustical Society of America, 2007, 122(2): 848-859.
[13] Suzuki T, Day B J. Comparative Study on Mode-Identification Algorithms Using a Phased-Array System in a Rectangular Duct[J]. Journal of Sound & Vibration, 2015, 347(7): 27-45.
[14] Sijtsma P, Zillmann J. In-Duct and Far-Field Mode Detection Techniques[R]. AIAA 2007-3439.
[15] Blacodon D. Spinning Mode Analysis of the Acoustic Field Generated by a Turboshaft Engine[J]. Journal of Aircraft, 2015, 29 (6): 1073-1079.
[16] Daniel L Sutliff. Turbofan Duct Mode Measurements Using a Continuously Rotating Microphone Rake[J]. International Journal of Aeroacoustics, 2007, 6(2): 147-170.
[17] Sutliff D L. Rotating Rake Turbofan Duct Mode Measurement System[J]. Journal of the Acoustical Society of America, 2005 , 118 (3): 1864-1864.
[18] Huang X. Compressive Sensing and Reconstruction in Measurements with an Aerospace Application[J]. AIAA Journal, 2013, 51(4): 1011-1016.
[19] Yu W, Huang X. Compressive Sensing Based Spinning Mode Detections by In-Duct Microphone Arrays[J]. Measurement Science & Technology, 2016, 27(5):055901.
[20] Zhou D, Wang X, Chen J, et al. Sound Generation by Non-Synchronously Oscillating Rotor Blades in Turbomachinery[J]. Journal of Sound & Vibration, 2015 , 355 : 150-171.
[21] Peake N, Parry A B. Modern Challenges Facing Turbomachinery Aeroacoustics[J]. Annual Review of Fluid Mechanics, 2011, 44 (1): 227-248.(编辑:朱立影) * 收稿日期:2017-06-20;修订日期:2017-08-20。基金项目:国家自然科学基金(51676008)。作者简介:李志彬,男,硕士,研究领域为气动声学。E-mail: lizhibin012@126.com通讯作者:王晓宇,女,博士,副教授,研究领域为气动声学。E-mail: bhwxy@buaa.edu.cn
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