Active Flow Control: Papers contributed to the Conference by Rudibert King

By Rudibert King

This publication includes contributions awarded on the energetic stream keep an eye on 2006 convention, held September 2006, on the Technische Universit?t Berlin, Germany. It incorporates a good balanced mixture of theoretical and experimental state of the art result of lively movement keep an eye on. insurance combines new advancements in actuator expertise, sensing, strong and optimum open- and closed-loop keep an eye on and version aid for regulate.

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Extra info for Active Flow Control: Papers contributed to the Conference Active Flow Control 2006, Berlin, Germany, September 27 to 29, 2006 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)

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6. 8 50 70 90 110 130 150 x /mm 130 120 110 100 90 80 70 60 50 40 30 20 10 0 -10 -20 Fig. 7. 6%. Frequency spectra for the tagged points are presented in Fig. 8. stall already at inclination angles of about α = 5◦ [38]. Consequently, the plate is in deep stall at α = 16◦ and the large separation zone on the suction side shown in Fig. 7 results. This recirculation region extends downstream far behind the trailing edge with the maximum of backflow situated in the aft position of the plate and rearward of the trailing edge.

3. 0 y /mm y /mm -2 20 20 40 40 60 60 80 80 60 80 100 120 140 160x /mm y /mm 40 y /mm 20 20 20 40 40 60 60 20 40 60 80 100 120 140 20 40 60 80 100 120 140 160x /mm 80 80 20 40 60 80 100 120 140 160x /mm 160x /mm Fig. 4. 5 and 4 is given. Phase averaging of the synchronized PIV data was performed based on the excitation frequency. One period has been split into 20 equally wide bins. In the first half period, the Lorentz force points downstream, while it changes sign in the second half period. 5, no discernible vortex structures can be found in Fig.

Applied Magnetohydrodynamics. Reports of the Physics Institute 12 (1961) 147–154 (in Russian). : Boundary layer control by means of wall parallel Lorentz forces. : Some results on electromagnetic control of flow around bodies. In: Int. Symp. on Seawater Drag Reduction. : Role of actuation frequency in controlled flow reattachement over a stalled airfoil. AIAA J. : On the identification of a vortex. J. Fluid Mech. : Aerodynamik des Flugmodells. Tragfl¨ugelmessungen I. E. Volckmann Nachf. E. Wette, Berlin–Charlottenburg (1942) Pulsed Plasma Actuators for Active Flow Control at MAV Reynolds Numbers B.

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