Abstract
A prediction model of the performance of circular synthetic jets in quiescent conditions is developed using both dimensional and quantitative analyses. This model provides analytical relations between the performance parameters (both dimensional and non-dimensional) and the operating parameters of synthetic jet actuators. The model is validated by a systematic numerical approach using 42 laminar flow cases which cover the dimensionless stroke length in the range of 1.13
Original language | English |
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Title of host publication | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers|Aeros. Sci. Meet. Exhib. Meet. Pap. |
Pages | 3953-3967 |
Number of pages | 14 |
Publication status | Published - 2005 |
Event | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV Duration: 1 Jul 2005 → … |
Conference
Conference | 43rd AIAA Aerospace Sciences Meeting and Exhibit |
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City | Reno, NV |
Period | 1/07/05 → … |