Citation: | XIANG Honghui, GAO Jie, YANG Rongfei, LIU Haixu, WU Senlin. Effect of probe support wake on vibration characteristics of compressor rotor blade[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(2): 58-66. DOI: 10.11729/syltlx20200070 |
[1] |
JONES M J, BIRCH N T, BRADBROOK S J. Evolutions in aircraft engine design and a vision for the future[R]. ISABE-2002-1014, 2001.
|
[2] |
BROICHHAUSEN K D, ZIEGLER K U. Supersonic and transonic compressors: past, status and technology trends[C]//Proceedings of ASME Turbo Expo 2005: Power for Land, Sea, and Air. 2008. doi: 10.1115/GT2005-69067
|
[3] |
MILLER R J, MOSS R W, AINSWORTH R W, et al. Time-resolved vane-rotor interaction in a high-pressure turbine stage[J]. Journal of Turbomachinery, 2003, 125(1): 1-13. doi: 10.1115/1.1492823
|
[4] |
王英锋, 胡骏, 李传鹏, 等. 上游转子对下游静子叶片气动力的影响[J]. 航空学报, 2006, 27(4): 545-550. DOI: 10.3321/j.issn:1000-6893.2006.04.001
WANG Y F, HU J, LI C P, et al. Effects of up-stream rotor on the aerodynamic force on down-stream stator blades[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(4): 545-550. doi: 10.3321/j.issn:1000-6893.2006.04.001
|
[5] |
DUDZINSKI T J, KRAUSE L N. Effect of inlet geometry on flow-angle characteristics of miniature total-pressure tubes[R]. NASA TN D-6460, 1971.
|
[6] |
COLDRICK S, IVEY P, WELLS R. Considerations for using 3D pneumatic probes in high speed axial compressors[C]//Proceedings of ASME Turbo Expo 2002: Power for Land, Sea, and Air. 2009. doi: 10.1115/GT2002-30045
|
[7] |
LEPICOVSKY J. Effects of a rotating aerodynamic probe on the flow field of a compressor rotor[R]. NASA/CR-2008-215215, 2008.
|
[8] |
MA H W, LI S H, WEI W. Effects of probe support on the flow field of a low-speed axial compressor[J]. Journal of Thermal Science, 2014, 23(2): 120-126. doi: 10.1007/s11630-014-0685-7
|
[9] |
MA H W, LI S H, WEI W. Effects of probe support on the stall characteristics of a low-speed axial compressor[J]. Journal of Thermal Science, 2016, 25(1): 43-49. doi: 10.1007/s11630-016-0832-4
|
[10] |
HE X, MA H W, REN M L, et al. Investigation of the effects of airfoil-probes on the aerodynamic performance of an axial compressor[J]. Chinese Journal of Aeronautics, 2012, 25(4): 517-523. doi: 10.1016/S1000-9361(11)60415-9
|
[11] |
XIANG H H, GE N, HOU M J, et al. An experimental investigation of the effects of upstream probe disturbance on compressor cascade performance[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231(7): 1248-1257. doi: 10.1177/0954410016652435
|
[12] |
XIANG H H, GE N, GAO J, et al. Experimental investigation of the effect of the probe support tail structure on the compressor cascade flow field[J]. International Journal of Turbo & Jet-Engines, 2019, 36(1): 9-18. doi: 10.1515/tjj-2016-0071
|
[13] |
WISLER D C. Core compressor exit stage study. Volume 3: Data and performance report for screening test configurations[R]. NASA CR-159499, 1980.
|
[14] |
KENYON J A, RABE D C, FLEETER S. Aerodynamic effects on blade vibratory stress variations[J]. Journal of Propulsion and Power, 1999, 15(5): 675-680. doi: 10.2514/2.5492
|
[15] |
张明明, 侯安平, 贺小帆, 等. 进气畸变下压气机叶片强度分析[J]. 航空动力学报, 2011, 26(1): 108-114. DOI: 10.13224/j.cnki.jasp.2011.01.015
ZHANG M M, HOU A P, HE X F, et al. Intensity analysis of blades in axial compressor with inlet distortion[J]. Journal of Aerospace Power, 2011, 26(1): 108-114. doi: 10.13224/j.cnki.jasp.2011.01.015
|
[16] |
SRINIVASAN A V. Flutter and resonant vibration characteristics of engine blades: an IGTI scholar paper[C]//Proceedings of ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. 2014. doi: 10.1115/97-GT-533
|
[17] |
EKICI K, VOYTOVYCH D, HALL K. Time-linearized navier-stokes analysis of flutter in multistage turbomachines[C]//Proc of the 43rd AIAA Aerospace Sciences Meeting and Exhibit. 2005. doi: 10.2514/6.2005-836
|
[18] |
张明明, 李绍斌, 侯安平, 等. 叶轮机械叶片颤振研究的进展与评述[J]. 力学进展, 2011, 41(1): 26-38. https://www.cnki.com.cn/Article/CJFDTOTAL-LXJZ201101004.htm
ZHANG M M, LI S B, HOU A P, et al. A review of the research on blade flutter in turbomachinery[J]. Advances in Mechanics, 2011, 41(1): 26-38. https://www.cnki.com.cn/Article/CJFDTOTAL-LXJZ201101004.htm
|
[19] |
DICKMANN H P, SECALL WIMMEL T, SZWEDOWICZ J, et al. Unsteady flow in a turbocharger centrifugal compressor: three-dimensional computational fluid dynamics simulation and numerical and experimental analysis of impeller blade vibration[J]. Journal of Turbomachinery, 2006, 128(3): 455-465. doi: 10.1115/1.2183317
|
[20] |
闫嘉超, 侯安平, 周盛. 非定常耦合流动对叶片动力响应的影响[J]. 航空动力学报, 2010, 25(3): 582-586. DOI: 10.13224/j.cnki.jasp.2010.03.011
YAN J C, HOU A P, ZHOU S. Effect of unsteady cooperative flow on the dynamic response in the rotor of axial compressor[J]. Journal of Aerospace Power, 2010, 25(3): 582-586. doi: 10.13224/j.cnki.jasp.2010.03.011
|
1. |
鄂东梅. 真空技术在航空航天中的应用. 真空. 2021(03): 77-81 .
![]() | |
2. |
邓小龙,杨希祥,麻震宇,朱炳杰,侯中喜. 基于风场环境利用的平流层浮空器区域驻留关键问题研究进展. 航空学报. 2019(08): 23-36 .
![]() |