Study of synthetic jets in boundary layers

As a zero-net-mass-flux actuator, a synthetic jet (SJ) actuator is a promising active flow separation control device. In order to make this technology more feasible in real-world applications, this research aims to uncover more underlying physics associated with SJ-based flow separation control. Bot...

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Bibliographic Details
Main Author: Wen, Xin
Other Authors: Tang Hui
Format: Thesis
Language:English
Published: 2015
Subjects:
Online Access:https://hdl.handle.net/10356/64554
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author Wen, Xin
author2 Tang Hui
author_facet Tang Hui
Wen, Xin
author_sort Wen, Xin
collection NTU
description As a zero-net-mass-flux actuator, a synthetic jet (SJ) actuator is a promising active flow separation control device. In order to make this technology more feasible in real-world applications, this research aims to uncover more underlying physics associated with SJ-based flow separation control. Both a CFD framework and a water-tunnel platform are developed, and decomposition methods are applied to extract coherent flow structures. It is found that the single-SJ-induced hairpin vortex in the turbulent boundary layer (TBL) is asymmetric, oscillates laterally, and dissipates fast, whereas it is symmetric and persistent in the laminar boundary layer (LBL). Using in line twin SJs in attached LBLs, three types of vortex structures are identified at various operational phase differences: one combined vortex at 90 degree, two completely separated vortices at 270 degree, and partially interacting vortex structures at 0 and 180 degree. Distinct flow control effect is found by applying these vortex structures on a separated LBL.
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spelling ntu-10356/645542023-03-11T17:53:36Z Study of synthetic jets in boundary layers Wen, Xin Tang Hui Fei Duan School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering::Fluid mechanics As a zero-net-mass-flux actuator, a synthetic jet (SJ) actuator is a promising active flow separation control device. In order to make this technology more feasible in real-world applications, this research aims to uncover more underlying physics associated with SJ-based flow separation control. Both a CFD framework and a water-tunnel platform are developed, and decomposition methods are applied to extract coherent flow structures. It is found that the single-SJ-induced hairpin vortex in the turbulent boundary layer (TBL) is asymmetric, oscillates laterally, and dissipates fast, whereas it is symmetric and persistent in the laminar boundary layer (LBL). Using in line twin SJs in attached LBLs, three types of vortex structures are identified at various operational phase differences: one combined vortex at 90 degree, two completely separated vortices at 270 degree, and partially interacting vortex structures at 0 and 180 degree. Distinct flow control effect is found by applying these vortex structures on a separated LBL. DOCTOR OF PHILOSOPHY (MAE) 2015-05-28T03:22:57Z 2015-05-28T03:22:57Z 2015 2015 Thesis Wen, X. (2015). Study of synthetic jets in boundary layers. Doctoral thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/64554 10.32657/10356/64554 en 174 p. application/pdf
spellingShingle DRNTU::Engineering::Mechanical engineering::Fluid mechanics
Wen, Xin
Study of synthetic jets in boundary layers
title Study of synthetic jets in boundary layers
title_full Study of synthetic jets in boundary layers
title_fullStr Study of synthetic jets in boundary layers
title_full_unstemmed Study of synthetic jets in boundary layers
title_short Study of synthetic jets in boundary layers
title_sort study of synthetic jets in boundary layers
topic DRNTU::Engineering::Mechanical engineering::Fluid mechanics
url https://hdl.handle.net/10356/64554
work_keys_str_mv AT wenxin studyofsyntheticjetsinboundarylayers