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Numerical analysis of 3-D sound propagation in lined ducts with circumferential mode sound sources at inlet
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作者 ZHU Zhichi and WU Jinlong( Tsinghua University ) 《Chinese Journal of Acoustics》 1991年第2期111-118,共8页
Numerical analysis of three-dimensional sound propagation in soft-soft or soft-hard circular ducts with circumferential and axial modes of sound sources at the inlet has been carried out. In this paper , the numerical... Numerical analysis of three-dimensional sound propagation in soft-soft or soft-hard circular ducts with circumferential and axial modes of sound sources at the inlet has been carried out. In this paper , the numerical method and the samples are offered and the effects of circumferential and axial modes on numerical results are discussed in detail . 展开更多
关键词 Numerical analysis of 3-D sound propagation in lined ducts with circumferential mode sound sources at inlet mode
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Modal Analysis of Axial Compressor Tip Rotating Instability under Varying Operating Conditions 被引量:2
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作者 LI Tao WU Yadong +1 位作者 TIAN Jie OUYANG Hua 《Journal of Thermal Science》 SCIE EI CAS CSCD 2023年第4期1345-1356,共12页
The full annulus numerical research was performed on a low-speed compressor rotor to investigate the rotating instability in the tip region.The frequency spectra show the existence of rotating instability at narrow st... The full annulus numerical research was performed on a low-speed compressor rotor to investigate the rotating instability in the tip region.The frequency spectra show the existence of rotating instability at narrow stable operating range.With the decrease of flow rate,31 cells of flow disturbance can be found in the instantaneous flow field.The distribution of vortex suggests that the circumferential propagation of the interaction between tip leakage vortex and adjacent blade brings about these cells.The dynamic mode decomposition(DMD)method and spatial discrete Fourier transform(SDFT)were applied to obtain the circumferential mode features,and the results indicate that the rotating instability is associated with the 31 cells of flow disturbance.Then the DMD method was further applied on the pressure data from a circle and an annulus domain,so as to extract different mode components with the corresponding spatial structures,frequencies and amplitudes.The results suggest that DMD modes can display the flow feature and explore the evolution of each instability source in the tip flow field. 展开更多
关键词 axial compressor rotating instability flow structure circumferential mode dynamic mode decomposition
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