A synthetic jet evolving in a boundary layer with laminar separation

Tsang, P; Hong, G

A synthetic jet evolving in a boundary layer with laminar separation

Tsang, P Hong, G

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Publication Type:: Journal Article
Citation:: Journal of Flow Visualization and Image Processing, 2010, 17 (3), pp. 229 - 242
Issue Date:: 2010-01-01

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Field	Value	Language
dc.contributor.author	Tsang, P	en_US
dc.contributor.author	Hong, G https://orcid.org/0000-0002-1905-1161	en_US
dc.date.issued	2010-01-01	en_US
dc.identifier.citation	Journal of Flow Visualization and Image Processing, 2010, 17 (3), pp. 229 - 242	en_US
dc.identifier.issn	1065-3090	en_US
dc.identifier.uri	http://hdl.handle.net/10453/15295
dc.description.abstract	This paper reports our work on numerical modeling of a micro synthetic jet in a boundary layer with flow separation caused by an adverse pressure gradient. The numerical model was developed using a commercial code with three-dimensional Large Eddy Simulation (LES) being applied. The model was verified by experimental results. The numerical results enabled flow visualization which helped us understand the evolution of a synthetic jet between the synthetic jet actuator (SJA) and the onset of separation, which was not measured in the experiments. © 2010 by Begell House, Inc.	en_US
dc.relation.ispartof	Journal of Flow Visualization and Image Processing	en_US
dc.relation.isbasedon	10.1615/JFlowVisImageProc.v17.i3.40	en_US
dc.subject.classification	Mechanical Engineering & Transports	en_US
dc.title	A synthetic jet evolving in a boundary layer with laminar separation	en_US
dc.type	Journal Article
utslib.citation.volume	3	en_US
utslib.citation.volume	17	en_US
utslib.for	0913 Mechanical Engineering	en_US
utslib.for	091305 Energy Generation, Conversion and Storage Engineering	en_US
pubs.embargo.period	Not known	en_US
pubs.organisational-group	/University of Technology Sydney
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Mechanical and Mechatronic Engineering
utslib.copyright.status	closed_access
pubs.issue	3	en_US
pubs.publication-status	Published	en_US
pubs.volume	17	en_US

Abstract:

This paper reports our work on numerical modeling of a micro synthetic jet in a boundary layer with flow separation caused by an adverse pressure gradient. The numerical model was developed using a commercial code with three-dimensional Large Eddy Simulation (LES) being applied. The model was verified by experimental results. The numerical results enabled flow visualization which helped us understand the evolution of a synthetic jet between the synthetic jet actuator (SJA) and the onset of separation, which was not measured in the experiments. © 2010 by Begell House, Inc.

Please use this identifier to cite or link to this item:

http://hdl.handle.net/10453/15295