Abstract
Adaptive closed-loop control of flow separation over a non-slotted flap is proposed in this paper. It is implemented through optimization of either the forcing frequency or the oscillatory momentum coeffcient. First, to optimize the forcing frequency, a modified extremum-seeking scheme involving the local estimation of the equilibrium map curvature and a fuzzy regulator is developed. On this application, the modified scheme shows faster convergence rate than the classic one. Secondly, to optimize the oscillatory momentum coeffcient, a modified slope-seeking scheme is proposed. It involves a fuzzy-logic regulator to compensate the equilibrium map local gradient variations and this enables faster convergence rate than the classic slope-seeking scheme.
| Original language | English |
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| DOIs | |
| Publication status | Published - 1 Jan 2013 |
| Externally published | Yes |
| Event | 31st AIAA Applied Aerodynamics Conference - San Diego, CA, United States Duration: 24 Jun 2013 → 27 Jun 2013 |
Conference
| Conference | 31st AIAA Applied Aerodynamics Conference |
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| Country/Territory | United States |
| City | San Diego, CA |
| Period | 24/06/13 → 27/06/13 |