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Xu Hangshou, Kang Zhongxu, Ji Zhenlin. Experimental of axial compressor[J]. Journal of Aerospace Power, 2019,
measurement and analysis of transmission loss of exhaust 34(1): 156–167.
silencers[J]. Noise and Vibration Control, 2009, 29(4): [10] Williams E G. Regularization methods for near-field
128–131. acoustical holography[J]. The Journal of Acoustical So-
[3] Felix S, Pagneux V. Sound propagation in rigid bends: a ciety of America, 2001, 110(4): 1976–1988.
multimodal approach[J]. The Journal of Acoustical Soci- [11] Wu S F. Reconstructing transient acoustic radiation from
ety of America, 2001, 110(3 Pt 1): 1329–1337. an arbitrary object with a uniform surface velocity distri-
[4] Bi W, Pagneux V, Lafarge D, et al. An improved multi- bution[J]. The Journal of Acoustical Society of America,
modal method for sound propagation in nonuniform lined
2014, 136(2): 514–524.
ducts[J]. The Journal of Acoustical Society of America,
[12] Hald J. Basic theory and properties of statistically opti-
2007, 122(1): 280–290.
mized near-field acoustical holography[J]. The Journal of
[5] Kooijmana G, Testudb P, Aureganc Y, et al. Multimodal
Acoustical Society of America, 2009, 125: 2105–2120.
method for scattering of sound at a sudden area expan-
[13] Wu H, Jiang W. Experimental study of the mapping rela-
sion in a duct with subsonic flow[J]. Journal of Sound and
tionship based near-field acoustic holography with spheri-
Vibration, 2008, 310(4/5): 902–922.
cal fundamental solutions[J]. Journal of Sound and Vibra-
[6] 夏烨. 浅析大涵道比涡扇发动机管道声模态测试技术 [C]. 面
tion, 2017, 394: 185–202.
向航空试验测试技术——2013 年航空试验测试技术峰会暨学
[14] Brooks T F, Humphreys W M. A deconvolution approach
术交流会论文集, 2013, 32: 90–93.
[7] 梁东, 王利, 弓志强, 等. 一种风扇/压气机声模态测量分析方 for the mapping of acoustic sources (DAMAS) determined
from phased microphone arrays[J]. The Journal of Acous-
法 [J]. 燃气涡轮试验与研究, 2015, 28(3): 49–53, 62.
Liang Dong, Wang Li, Gong Zhiqiang, et al. Research tical Society of America, 2006, 294(4/5): 856–879.
on acoustic mode measurement analysis method for a fan/ [15] Sijtsma P, Merino-Martinez R, Malgoezar A M N. High-
compressor[J]. Gas Turbine Experiment and Research, resolution CLEAN-SC: theory and experimental vali-
2015, 28(3): 49–53, 62. dation[J]. International Journal of Aeroacoustics, 2017,
[8] 王良锋. 风扇管道声模态识别的实验及数值模拟研究 [D]. 西 16(4/5): 274–298.
安: 西北工业大学出版社, 2017. [16] Hua X, Jiang C, Herrin D W, et al. Determination of
[9] 肖志成, 田杰, 姚丹, 等. 压缩感知在轴流压气机周向模态识 transmission and insertion loss for multi-inlet mufflers us-
别中的应用 [J]. 航空动力学报, 2019, 34(1): 156–167. ing impedance matrix and superposition approaches with
Xiao Zhicheng, Tian Jie, Yao Dan, et al. Application of comparisons[J]. Journal of Sound and Vibration, 2014,
compressed sensing in circumferential modal identification 333(22): 5680–5692.