Abstract
Flow field generated in and around micro synthetic jet actuator is analyzed using the an existing Navier-Stokes solver. The solver is modified to accomodate 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 distributions well as the flow field inside the cavity.
Original language | English |
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Title of host publication | RAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies |
Editors | S. Kurnaz, Fuat Ince, S. Onbasioglu |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 582-586 |
Number of pages | 5 |
ISBN (Electronic) | 0780381424, 9780780381421 |
DOIs | |
Publication status | Published - 2003 |
Event | International Conference on Recent Advances in Space Technologies, RAST 2003 - Istanbul, Turkey Duration: 20 Nov 2003 → 22 Nov 2003 |
Publication series
Name | RAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies |
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Conference
Conference | International Conference on Recent Advances in Space Technologies, RAST 2003 |
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Country/Territory | Turkey |
City | Istanbul |
Period | 20/11/03 → 22/11/03 |
Bibliographical note
Publisher Copyright:© 2003 IEEE.