[1] Holzinger F., Wartzek F., Nestle M., et al., Self-excited blade vibration experimentally investigated in transonic compressors–rotating instabilities and flutter. Journal of Turbomachinery, 2016, 138(4): 041006.
[2] Han L., Wei D.S., Wang Y.R., et al., Analysis method of nonsynchronous vibration and influence of tip clearance flow instabilities on non-synchronous vibration in an axial transonic compressor rotor. Journal of Turbomachinery, 2021, 143(11): 111014.
[3] Zhao T.T., Jing X.D., Sha Y.D., et al., Analysis of noise characteristics and acoustic structure coupling mechanism of rotor blades in compressor. Acta Aeronautica et Astronautica Sinica, 2019, 40(5): 124–133.
[4] Chen W.X., Wang Y.G., Wang H., Investigation of the unsteady disturbance in tip region of a contra-rotating compressor near stall. Journal of Thermal Science, 2019, 28(5): 962–974.
[5] Holzinger F., Wartzek F., Nestle M., at al., Self-excited blade vibration experimentally investigated in transonic compressors: acoustic resonance. Journal of Turbomachinery, 2016, 138(4): 0411001.
[6] Wang H., Wu Y.D., Yue S.Y., et al., Numerical investigation on the flow mechanism of multi-peak frequency feature of rotating instability. Journal of Thermal Science, 2021, 30(2): 668–681.
[7] Li T., Wu Y.D., Tian J., et al., Modal analysis of axial compressor tip rotating instability under varying operating conditions. Journal of Thermal Science, 2023, 32(4): 1345–1356.
[8] Baumgartner M., Kamerier F., Hourmouziadis J., Non-engine order blade vibration in a high pressure compressor. Twelfth international symposition on air breathing engines, Melbourne, Australia, 1995.
[9] Im H., Zha G.C., Investigation of flow instability mechanism causing compressor rotor-blade nonsynch- ronous vibration. AIAA Journal, 2014, 52(9): 2019–2031.
[10] Ciorciari R., Lesser A., Blaim F., et al., Numerical investigation of tip clearance effects in an axial transonic compressor. Journal of Thermal Science, 2012, 21(2): 109–119.
[11] Mailach R., Lehmann I., Vogeler K., Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex. Journal of Turbomachinery, 2001, 119(3): 453–460.
[12] Im H., Zha G.C., Effects of rotor tip clearance of tip clearance flow potentially leading to NSV in an axial compressor. ASME Turbo Expo, Copenhagen, Denmark, Paper NO. GT2012-68148.
[13] Yang Z.Y., Wu Y.D., Liu Z.L., et al., Tip flow on rotating instability on an axial compressor with different tip clearance. Aerospace Science and Technology, 2023, 139: 108364
[14] Thomassin J., Vo H.D., Mureithi N.W., Blade tip clearance flow and compressor NSV: the jet core feedback as the coupling mechanism. ASME Turbo Expo, Paper No. GT2007-27286.
[15] Thomassin J., Vo H.D., Mureithi N.W., Experimental demonstration: of the tip clearance flow resonance behind compressor non-synchronous vibration. ASME Turbo Expo: Power for Land, Sea, and Air - Berlin, Germany, Paper NO. GT2008-50303.
[16] Thomassin J., Vo H.D., Mureithi N.W., The tip clearance flow resonance behind axial compressor non-synchronous vibration. Journal of Turbomachinery, 2011, 133(4): 041030.
[17] Vo H.D., Tan C.S., Greitzer E.M., Criteria for spike initiated rotating stall. Journal of Turbomachinery, 2008, 130(1): 011023.
[18] Drolet M., Thomassin J., Vo H.D., et al., Numerical investigation into non-synchronous vibrations of axial flow compressors by the resonant tip clearance flow. ASME Turbo Expo, Paper No. GT2009-59074.
[19] Drolet M., Vo H.D., Mureithi N.W., Effect of tip clearance on the prediction of non-synchronous vibrations in axial compressor. ASME Turbo Expo, Paper No. GT2011-45392.
[20] Kielb R.E., Thomas J.P., Barter J.W., et al., Blade excitation by aerodynamic instabilities: a compressor blade study. ASME Turbo Expo, Paper No. GT2003- 38634.
[21] Im H., Zha G.C., Simulation of non-synchronous blade vibration of an axial compressor using a fully coupled fluid/structure interaction. ASME Turbo Expo, Paper No. GT2012-68150.
[22] Im H., Zha G.C., Effects of rotor tip clearance on tip clearance flow potentially leading to NSV in an axial compressor. ASME, Paper No. GT2012-68148.
[23] Gan J.Y., Im H., Zha G.C., Investigation of a compressor rotor non-synchronous vibration with and without fluid-structure interaction. ASME, Paper No. GT2014-26478.
[24] Zhu X. C., Hu P., Lin T., et al., Numerical investigations on non-synchronous vibration and frequency lock-in of low pressure steam turbine last stage. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2022, 236(4): 647–661.
[25] Stapelfeldt S., Brandstetter C., Non-synchronous vibration in axial compressors: lock-in mechanism and semi-analytical model. Journal of Sound and Vibration, 2020, 488(11): 115649.
[26] Gan J.Y., Im H., Zha G.C., Numerical examination of lock-in hypothesis of non-synchronous vibration in an axial compressor. ASME Turbo Expo, Paper No. GT2017-65244.
[27] Zheng Y., Gao Q., Yang H., Non-synchronous blade vibration analysis of a transonic fan. Chinese Journal of Aeronautics, 2023, 36(1): 178–190.
[28] Kameier F., Neise W., Rotating blade flow instability as a source of noise in axial turbomachines. Journal of Sound and Vibration, 1997, 203(5): 833–853.
