Influence of synthetic jet location on boundary layer separation control

Lee, C; Hong, G; Mallinson, SG

Influence of synthetic jet location on boundary layer separation control

Lee, C Hong, G

Mallinson, SG

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Publication Type:: Conference Proceeding
Citation:: Proceedings of SPIE - The International Society for Optical Engineering, 2004, 5276 pp. 230 - 239
Issue Date:: 2004-06-01

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Field	Value	Language
dc.contributor.author	Lee, C	en_US
dc.contributor.author	Hong, G https://orcid.org/0000-0002-1905-1161	en_US
dc.contributor.author	Mallinson, SG https://orcid.org/0000-0003-1323-1062	en_US
dc.date.issued	2004-06-01	en_US
dc.identifier.citation	Proceedings of SPIE - The International Society for Optical Engineering, 2004, 5276 pp. 230 - 239	en_US
dc.identifier.issn	0277-786X	en_US
dc.identifier.uri	http://hdl.handle.net/10453/7252
dc.description.abstract	When synthetic jet actuators are used to control flow separation in practical situations, it is anticipated that the orifices will be distributed in the form of an array. Wind tunnel experiments were conducted to investigate the effect of the location and number of these actuators on boundary layer separation. Three synthetic jets were located upstream of the separation point in undisturbed flow, and the mean and root mean-square (RMS) velocity profiles were measured at several axial locations within the separated flow region. This paper reports the effect of actuator placement and the integrated effectiveness of two and three synthetic jets with different forcing voltages and frequencies.	en_US
dc.relation.ispartof	Proceedings of SPIE - The International Society for Optical Engineering	en_US
dc.relation.isbasedon	10.1117/12.523270	en_US
dc.title	Influence of synthetic jet location on boundary layer separation control	en_US
dc.type	Conference Proceeding
utslib.citation.volume	5276	en_US
utslib.for	090101 Aerodynamics (excl. Hypersonic Aerodynamics)	en_US
utslib.for	091305 Energy Generation, Conversion and Storage Engineering	en_US
dc.location.activity	Perth, Australia	en_US
dc.location.activity	Univ Western Australia, Perth, AUSTRALIA
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.publication-status	Published	en_US
pubs.volume	5276	en_US

Abstract:

When synthetic jet actuators are used to control flow separation in practical situations, it is anticipated that the orifices will be distributed in the form of an array. Wind tunnel experiments were conducted to investigate the effect of the location and number of these actuators on boundary layer separation. Three synthetic jets were located upstream of the separation point in undisturbed flow, and the mean and root mean-square (RMS) velocity profiles were measured at several axial locations within the separated flow region. This paper reports the effect of actuator placement and the integrated effectiveness of two and three synthetic jets with different forcing voltages and frequencies.

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http://hdl.handle.net/10453/7252