Axial compressor blades tip leakage flow control using natural aspiration

Abstract Blades tip leakage flow structure in axial compressors has dominant effects on flow stability and losses. Accordingly, in the present study, three different ideas are introduced for alleviation of undesirable effects of the blades tip leakage flow. These ideas utilize circumferential tape,...

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Main Authors: Peyman Ghashghaie Nejad, Reza Taghavi Zenouz
Format: Article
Language:English
Published: Nature Portfolio 2023-12-01
Series:Scientific Reports
Online Access:https://doi.org/10.1038/s41598-023-49391-9
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author Peyman Ghashghaie Nejad
Reza Taghavi Zenouz
author_facet Peyman Ghashghaie Nejad
Reza Taghavi Zenouz
author_sort Peyman Ghashghaie Nejad
collection DOAJ
description Abstract Blades tip leakage flow structure in axial compressors has dominant effects on flow stability and losses. Accordingly, in the present study, three different ideas are introduced for alleviation of undesirable effects of the blades tip leakage flow. These ideas utilize circumferential tape, S-shape nozzle and natural aspiration slot, all imposed upstream the rotor blades row. The method of investigation is based on numerical simulation of the governing flow field. Results, in terms of the flow field structure and performance curves are compared with those of the untreated case. Final results, showed that the natural aspiration idea works better than the other ones. In comparison to the plane case, it is accompanied by augmentation of 3.5% in the total pressure ratio and 3% in the surge margin. It was also found that the mass flow rate passing through the blades row tip gap has increased by 2.33 g/s in the natural aspiration case.
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spelling doaj.art-e32c62de57d94bd9b4d85d13c3cadb7c2023-12-24T12:14:19ZengNature PortfolioScientific Reports2045-23222023-12-0113111110.1038/s41598-023-49391-9Axial compressor blades tip leakage flow control using natural aspirationPeyman Ghashghaie Nejad0Reza Taghavi Zenouz1School of Mechanical Engineering, Iran University of Science and Technology (IUST)School of Mechanical Engineering, Iran University of Science and Technology (IUST)Abstract Blades tip leakage flow structure in axial compressors has dominant effects on flow stability and losses. Accordingly, in the present study, three different ideas are introduced for alleviation of undesirable effects of the blades tip leakage flow. These ideas utilize circumferential tape, S-shape nozzle and natural aspiration slot, all imposed upstream the rotor blades row. The method of investigation is based on numerical simulation of the governing flow field. Results, in terms of the flow field structure and performance curves are compared with those of the untreated case. Final results, showed that the natural aspiration idea works better than the other ones. In comparison to the plane case, it is accompanied by augmentation of 3.5% in the total pressure ratio and 3% in the surge margin. It was also found that the mass flow rate passing through the blades row tip gap has increased by 2.33 g/s in the natural aspiration case.https://doi.org/10.1038/s41598-023-49391-9
spellingShingle Peyman Ghashghaie Nejad
Reza Taghavi Zenouz
Axial compressor blades tip leakage flow control using natural aspiration
Scientific Reports
title Axial compressor blades tip leakage flow control using natural aspiration
title_full Axial compressor blades tip leakage flow control using natural aspiration
title_fullStr Axial compressor blades tip leakage flow control using natural aspiration
title_full_unstemmed Axial compressor blades tip leakage flow control using natural aspiration
title_short Axial compressor blades tip leakage flow control using natural aspiration
title_sort axial compressor blades tip leakage flow control using natural aspiration
url https://doi.org/10.1038/s41598-023-49391-9
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AT rezataghavizenouz axialcompressorbladestipleakageflowcontrolusingnaturalaspiration