Numerical Investigation of the Effect of Hub Gaps on the 3D Flows Inside the Stator of a Highly Loaded Axial Compressor Stage

Guangfeng An, Zhu Fan, Ying Qiu, Ruoyu Wang, Xianjun Yu and Baojie Liu
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Guangfeng An: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
Zhu Fan: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
Ying Qiu: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
Ruoyu Wang: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
Xianjun Yu: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China
Baojie Liu: Research Institute of Aero-Engine, Beihang University, Beijing 102206, China

Energies, 2022, vol. 15, issue 19, 1-20

Abstract: Both the compressor performance and the 3D flows inside the stator passage are significantly impacted by the stator hub gap. The interplay between leakage flow and corner separation within a cantilevered stator of a highly loaded, low-speed axial compressor with a succession of stator hub gaps was examined numerically in this paper. Firstly, the simulated results were compared with the measured results, including the compressor characteristics, the 3D flow structures, and the flow fields at the stator outlet. The results revealed that the used CFD solver, as well as the corresponding setup, can reproduce the flow not only in terms of the trend along with the stator hub gap, but also in terms of the specific scale of the 3D flow structure. Hence, it is feasible enough to be applied in the present investigation. Secondly, the flow mechanisms of the interplay between the corner separation and the leakage flow with different stator hub gaps were analyzed. It was found that the velocity of the leakage flow is the key parameter that dominates the flow structures as well as the compressor performance. Additionally, a simple metric was proposed to be used to choose the optimum stator hub gap. By comparing our results with those from published research, this metric was proven to be feasible. Finally, it is also discussed how the stator hub gap affected the stator inlet flow and rotor performance. It is demonstrated that the stator passage flow blockage can affect the upstream flow field. As a result, the performance of the rotor tends to vary in the opposite direction to that of the stator.

Keywords: cantilevered stator; corner separation; leakage flow; optimum stator hub gap; axial compressors (search for similar items in EconPapers)
JEL-codes: Q Q0 Q4 Q40 Q41 Q42 Q43 Q47 Q48 Q49 (search for similar items in EconPapers)
Date: 2022
References: View complete reference list from CitEc
Citations: View citations in EconPapers (1)

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