Rotating Stall Inception Due to Breakdown of Tip Leakage Vortex in Compressor Rotors
Rotating Stall Inception Due to Breakdown of Tip Leakage Vortex in Compressor Rotors
批准号:
12650172
负责人:
FURUKAWA Masato
金额:
$2.37万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2000
资助国家:
日本
项目状态:
已结题
起止时间:
2000 至 2001
中文摘要
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英文摘要
The unsteady flow nature caused by the breakdown of the tip leakage vortex in an axial compressor rotor at near-stall conditions has been investigated by unsteady three-dimensional Navier-Stokes flow simulations and by experimental measurements. The simulations show that the spiral-type breakdown of the tip leakage vortex occurs inside the rotor passage at the near-stall conditions. Downstream of the breakdown onset, the tip leakage vortex twists and turns violently with time, thus interacting with the pressure surface of the adjacent blade. The motion of the vortex and its interaction with the pressure surface are cyclic. The vortex breakdown causes significant changes in the nature of the tip leakage vortex, which result in the anomalous phenomena in the time-averaged flow fields near the tip at the near-stall conditions: no rolling-up of the leakage vortex downstream of the rotor, disappearance of the casing wall pressure trough corresponding to the leakage vortex, large spread of t … More he low-energy fluid accumulating on the pressure side, and large pressure fluctuation on the pressure side. As the flow rate is decreased, the movement of the tip leakage vortex due to its breakdown becomes so large that the leakage vortex interacts with the suction surface as well as the pressure one. The interaction with the suction surface gives rise to the three-dimensional separation of the suction surface boundary layer.Unsteady full passage flow fields at a near-stall operating condition in the axial compressor rotor has been investigated by RANS simulation. The simulation has captured the nature of the rotating stall inception. It is found that the stall cell is part-span type and consists of a tornado-type separation vortex linking from blade suction surface near the tip to the casing. The spiral-type breakdown of the tip leakage vortex causes the interaction between the leakage vortex and the adjacent blade leading edge, thus resulting in the formation of the tornado-type vortex. Less
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古川雅人: "軸流圧縮機動翼の失速点近傍における翼端漏れ渦の崩壊に伴う異常流動現象"日本機械学会論文集,B編. 66-644. 1029-1037 (2000)
Masato Furukawa:“与轴流式压缩机转子叶片失速点附近的尖端泄漏涡流塌陷相关的异常流动现象”,日本机械工程师学会汇刊,B 版 66-644(2000 年)。 )
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Masato FURUKAWA: "Unsteady Flow Behavior due to Breakdown of Tip Leakage Vortex in a Axial Compressor Rotor Near-Stall Condition"ASME Paper. 2000-GT-666. 1-12 (2000)
Masato FURUKAWA:“轴流式压缩机转子近失速状态下叶尖泄漏涡流破坏导致的不稳定流动行为”ASME 论文。
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Masato FURUKAWA: "Anomalous Flow Phenomena Due to Breakdown of Tip Leakage Vortex in an Axial Compressor Rotor at Near-Stall Condition"Transactions of JSME, Series B. Vol. 66. 1029-1037 (2000)
古河正人:“近失速条件下轴流式压缩机转子中尖端泄漏涡流损坏导致的异常流动现象”JSME 交易,B 系列卷。
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Kazuhisa SAIKI: "Numerical Simulation of Tip Leakage Vortex Breakdown in Axial Compressor Rotors"Special Publication of National Aerospace Laboratory. SP-46. 295-300 (2000)
Kazuhisa SAIKI:“轴流式压缩机转子叶尖泄漏涡流破坏的数值模拟”国家航空航天实验室特刊。
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山田和豊: "軸流圧縮機の旋回失速初生時における非定常三次元渦流れ構造"日本機械学会第79期流体工学部門講演会論文集. 01(3). 97-97 (2001)
Kazutoyo Yamada:“轴流压缩机旋转失速开始时的不稳定三维涡流结构”日本机械工程师学会第 79 届流体工程分会会议记录 01(3) (2001)。
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共 11 条
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项目类别:Grant-in-Aid for Scientific Research (B)
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Assimilation of EFD and CFD in Analysis of Complex Internal Flow
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Broadband Noise Reduction by Controlling Vortex Structure in Turbomachinery Blade Row
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Effects of Tip Leakage Vortex Breakdown on Flow Field in Turbomachinery Blade Row
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