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

By Rudibert King

This publication includes contributions offered on the energetic stream keep watch over 2006 convention, held September 2006, on the Technische Universit?t Berlin, Germany. It encompasses a good balanced mixture of theoretical and experimental state of the art result of energetic movement keep watch over. assurance combines new advancements in actuator know-how, sensing, strong and optimum open- and closed-loop keep an eye on and version relief for keep watch over.

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Read Online or Download 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) PDF

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Extra resources 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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Fluid Mech. 360, pp. 179–211. , and Glezer, A. (1994) “Experimental Investigation of a Turbulent Jet Produced by an Oscillating Surface Actuator,” Appl. Mech. Rev. 47, no. 6, part 2, pp. S127– S1131. D. (1998) “Aircraft Laminar Flow Control,” Annu. Rev. Fluid Mech. 30, pp. 1–29. R. (1993a) “Two Nonlinear Control Schemes Contrasted in a Hydrodynamic Model,” Phys. Fluids A 5, pp. 931–947. R. (1993b) “Drag Reduction in Channel Flow Using Nonlinear Control,” AIAA Paper No. C. R. (1996) “A MEMS-Based Normal Vorticity Actuator for Near-Wall Modification of Turbulent Shear Flows,” Proc.

70, pp. 3031–3040. , and Mark, A. (1994b) “Experimental Control of Chaos for Communication,” Phys. Rev. Lett. 73, pp. 1781–1784. -C. (1996) “Review: MEMS and Its Applications for Flow Control,” J. Fluids Eng. 118, pp. 437–447. -C. (1998) “Micro-Electro-Mechanical Systems (MEMS) and Fluid Flows,” Annu. Rev. Fluid Mech. 30, pp. 579–612. , and Berkooz, G. (1996) Turbulence, Coherent Structures, Dynamical Systems and Symmetry, Cambridge University Press, Cambridge, Great Britain. 22 M. H. H. (1994) “Feedback Control to Delay or Advance Linear Loss of Stability in Planar Poiseuille Flow,” Proc.

It was driven by a frequency generator 33220A from Agilent. The applied Lorentz force strength is given as an effective momentum coefficient T 1 aB0 l cµ = · · · 2 2 ρU∞ c 1 T j(t)2 dt (7) 0 relating the rms momentum added by the Lorentz force to that in the free stream. In (7) j(t) denotes the time–depended current density, T its period of oscillation, and l the length of the actuator, respectively. For the plate investigated here l equals a. As common practice [3], we use percentage terms for cµ for convenience.

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