44th AIAA Aerospace Sciences Meeting and Exhibit 2006
DOI: 10.2514/6.2006-1401
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Adaptive Control of Separated Flow

Abstract: Adaptive closed-loop control is used to optimize the lift-to-drag ratio of post-stall separated flow over a NACA 0025 airfoil using multiple amplitudemodulated (AM) or burst-modulated (BM), zero-net-mass-flux (ZNMF) actuators that cover the central 33% span of the airfoil. A simplex optimization approach uses the lift and drag measured by a strain-gauge balance for feedback and searches for the optimal AM or BM actuation parameters in a closed-loop fashion. An energy penalty function based on the electrical po… Show more

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Cited by 40 publications
(35 citation statements)
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“…The amplitude of fluctuation is larger and then more difficult to be dissipated further downstream. Initially, it was expected that superposition or burst modulation are preferred if the objective is to act on two frequencies of the free flow (to act on the shear layer and wake instabilities as suggested by [14,29]). The present results highlight the non linear response of the actuator when it operates in ring modulation.…”
Section: Double Frequency Excitation: Ring Modulationmentioning
confidence: 99%
“…The amplitude of fluctuation is larger and then more difficult to be dissipated further downstream. Initially, it was expected that superposition or burst modulation are preferred if the objective is to act on two frequencies of the free flow (to act on the shear layer and wake instabilities as suggested by [14,29]). The present results highlight the non linear response of the actuator when it operates in ring modulation.…”
Section: Double Frequency Excitation: Ring Modulationmentioning
confidence: 99%
“…[1,14,15]. Therefore, the effect of thermal stratifications in complex terrain can be investigated as next step.…”
Section: Type Bmentioning
confidence: 99%
“…As first step, we will discuss the characteristics of the velocity profile in relation to the hill position. Following [1], we define a speed up effect as a velocity increase, and a blockage effect and an adverse pressure gradient effect as a velocity decrease at luv and lee, in each case in relation to the reference velocity profile over homogeneous surface.…”
Section: Type Bmentioning
confidence: 99%
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