Proceedings ArticleDOI
Unsteady Tip Clearance Flow in a Low-Speed Axial Compressor Rotor With Upstream and Downstream Stators
Xiangyang Deng,Hongwu Zhang,Jingyi Chen,Weiguang Huang +3 more
- pp 1371-1381
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In this article, the authors investigated the unsteady tip clearance flow in the second rotor of a two-stage low-speed axial compressor and its interaction with upstream and downstream stators.Abstract:
In the course of advancing the understanding of the unsteady flow nature of compressor tip clearance flows, the present paper investigates the unsteady tip clearance flow in the second rotor of a two-stage low-speed axial compressor and its interaction with upstream and downstream stators. Numerical methods were adopted in the present study and the research focused on clarifying the unsteadiness of tip clearance flow behavior and its link to the change of rotor performance, subjected to the variables of axial gap sizes between the rotor and upstream and downstream stators. The result shows how and why the tip leakage vortex trajectory changes its shape with the change of gap size, and its impact on the rotor pressure rise characteristic. Within all the computed operating range, the pressure rise increases monotonically with the decrease of upstream axial gaps, but no monotonic variation was observed with the change of downstream axial gaps. This trend of performance change could be explained by the unsteady effect of upstream stator wakes, and the overall result is that the rotor performance was found to be more influenced by the upstream interaction than the downstream interaction. The frequency characteristic of the tip clearance vortex, under the influence of gap size and compressor operating condition, was also analyzed to provide a quantified estimation of its periodic flow behavior and a comparison with the recent results of other researchers.Copyright © 2005 by ASMEread more
Citations
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Journal ArticleDOI
Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors
TL;DR: In this article, the authors used a collection of time-resolved pressure transducers on the casing with circumferential and chord-wise spatial resolution to observe the propagation of axial flow compressors.
Journal ArticleDOI
Effect of tip clearance and rotor–stator axial gap on the efficiency of a multistage compressor
Syed Noman Danish,Syed Noman Danish,Shafiq R. Qureshi,Malik Muhammad Imran,Salah Ud-Din Khan,Muhammad Mansoor Sarfraz,Abdelrahman El-Leathy,Abdelrahman El-Leathy,Hany Al-Ansary,Mingshan Wei +9 more
TL;DR: In this paper, the effect of tip clearance of rotor blades and axial gap between rotor and stator on the overall performance of a multistage axial compressor was investigated.
Proceedings ArticleDOI
Effects of Rotor Tip Blade Loading Variation on Compressor Stage Performance
TL;DR: Tan et al. as discussed by the authors assessed the effect of changing the rotor tip angle distribution on the performance of an embedded compressor stage and proposed a potential strategy for achieving a reduction in the loss generation.
Journal ArticleDOI
Investigation of tip leakage flow unsteadiness and rotating instability in a centrifugal compressor impeller
TL;DR: In this paper, a numerical analysis of rotating instability in a centrifugal compressor is presented, and it is shown that rotating instability can be found in axial compressors as well.
Journal ArticleDOI
Effects of Tip Leakage Flow on the Aerodynamic Performance and Stability of an Axial-Flow Transonic Compressor Stage
TL;DR: In this paper, the effect of tip leakage flow on the performance of axial flow transonic compressors was investigated numerically and the results showed that as the rotor tip clearance increases, the leakage flow intensity is increased, the shock wave position is moved backward, and the interaction between the tip leakage vortex and shock wave is intensified.