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Micro synthetic jets and their interaction with a cross flow in slip regime

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dc.contributor.authorEdis, F.O.
dc.contributor.authorErbas, N.
dc.contributor.authorBaysal, O.
dc.contributor.authorAslan, A.R.
dc.date.accessioned2026-01-25T00:04:37Z
dc.date.issued2003-01-01
dc.description.abstractThe flow field generated in and around a micro synthetic jet actuator is analyzed using the an existing Navier-Stokes solver. The solver is modified to accommodate slip wall boundary condition proposed in literature for micro scale flow problems. Two actuator cavity shapes, rectangular and triangular, are investigated for quiescent and cross-flow external domain conditions. Results are presented and compared for slip and no-slip conditions. Cavity shape is found to affect the orifice expulsion velocity profile. Cross-flow affects the orifice velocity distribution as well as the flow field inside the cavity.
dc.description.urihttps://doi.org/10.1109/rast.2003.1303981
dc.description.urihttps://dx.doi.org/10.1109/rast.2003.1303981
dc.identifier.doi10.1109/rast.2003.1303981
dc.identifier.endpage586
dc.identifier.openairedoi_dedup___::3b512c4ba8972d1caf6bb5de32ff2e90
dc.identifier.orcid0000-0003-0651-2181
dc.identifier.startpage582
dc.identifier.urihttps://hdl.handle.net/11527/40339
dc.publisherIEEE
dc.relation.ispartofInternational Conference on Recent Advances in Space Technologies, 2003. RAST '03. Proceedings of
dc.titleMicro synthetic jets and their interaction with a cross flow in slip regime
dc.typeArticle
dspace.entity.typePublication

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