Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit DesignSource: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003::page 31011-1DOI: 10.1115/1.4064078Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Sweeping jet (SJ) is a self-excited flow control device that can generate continuous and periodic flow, which makes it a promising geometry for film cooling. However, the cooling performance of current SJ configurations is not significantly better than that of 777-shaped holes. This paper presents two modified SJ configurations, named shaped SJ1 and shaped SJ2, which possess distinct shaped exit geometries. The spatiotemporal coolant distributions were comprehensively quantified for the 777-shaped hole, the compact SJ (with compact geometry), the shaped SJ1, and the shaped SJ2. The instantaneous cooling effectiveness distributions of the four configurations at blowing ratios (M) ranging from 0.5 to 3.0 were measured using the fast pressure-sensitive paint technique. The shaped SJ2 integrated the cooling characteristics of the 777-shaped hole and SJ. It maintained stability at a relatively low M, while began to oscillate when M was increased above 1.5. The shaped SJ design exhibited superior cooling effectiveness at both low and high M of 0.5 to 3.0. A proper orthogonal decomposition analysis and simulations illustrated the oscillation processes and flow structures within the SJ configuration. The shaped SJ2 showed a reduced outlet momentum and a more even distribution of film coverage than the 777-shaped hole, resulting in considerably improved cooling performance.
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contributor author | Wang, Kechen | |
contributor author | Zhou, Wenwu | |
contributor author | Wen, Xin | |
contributor author | Peng, Di | |
contributor author | Liu, Yingzheng | |
date accessioned | 2024-04-24T22:50:04Z | |
date available | 2024-04-24T22:50:04Z | |
date copyright | 12/14/2023 12:00:00 AM | |
date issued | 2023 | |
identifier issn | 0889-504X | |
identifier other | turbo_146_3_031011.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4295953 | |
description abstract | Sweeping jet (SJ) is a self-excited flow control device that can generate continuous and periodic flow, which makes it a promising geometry for film cooling. However, the cooling performance of current SJ configurations is not significantly better than that of 777-shaped holes. This paper presents two modified SJ configurations, named shaped SJ1 and shaped SJ2, which possess distinct shaped exit geometries. The spatiotemporal coolant distributions were comprehensively quantified for the 777-shaped hole, the compact SJ (with compact geometry), the shaped SJ1, and the shaped SJ2. The instantaneous cooling effectiveness distributions of the four configurations at blowing ratios (M) ranging from 0.5 to 3.0 were measured using the fast pressure-sensitive paint technique. The shaped SJ2 integrated the cooling characteristics of the 777-shaped hole and SJ. It maintained stability at a relatively low M, while began to oscillate when M was increased above 1.5. The shaped SJ design exhibited superior cooling effectiveness at both low and high M of 0.5 to 3.0. A proper orthogonal decomposition analysis and simulations illustrated the oscillation processes and flow structures within the SJ configuration. The shaped SJ2 showed a reduced outlet momentum and a more even distribution of film coverage than the 777-shaped hole, resulting in considerably improved cooling performance. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design | |
type | Journal Paper | |
journal volume | 146 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4064078 | |
journal fristpage | 31011-1 | |
journal lastpage | 31011-12 | |
page | 12 | |
tree | Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003 | |
contenttype | Fulltext |