By Petros Koumoutsakos, Igor Mezic
This rigorously edited monograph provides the state-of-the-art of idea and purposes in fluid move keep an eye on. It collects contributions via major specialists within the box of fluid circulate regulate attention-grabbing for engineers, physicists, or mathematicians on top of things and fluid dynamics. "Control of Fluid move" covers a variety of contemporary themes together with vortex established regulate algorithms, incompressible turbulent boundary layers, aerodynamic stream regulate, keep an eye on of combining and reactive movement strategies or nonlinear modeling and keep an eye on of combustion dynamics.
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Example text
Nishri, B. & Wygnanski, I. 1989 The delay of turbulent boundary layer separation by oscillatory active control. AIAA Paper 89–1027 . [40] Lin, J. C. 1999 Application of micro-vortex generators for turbulent flow separation control. In Mechanics of Passive and Active Flow Control (ed. G. E. A. Meier & P. R. Viswanath), Fluid Mechanics and its Applications, vol. 53, pp. 81–88. Dordrecht: Kluwer Acad. 98, Göttingen. [41] McCullough, G. B. & Gault, D. E. 1951 Examples of three representative types of airfoil-section stall at low speeds.
35] Isomoto, K. & Honami, S. 1989 The effect of inlet turbulence intensity on the reattachment process over a backward facing step. J. Fluids Eng. 111, 87–92, Transactions of the ASME. [36] Johnston, J. P. & Nishi, M. 1990 Vortex generator jets - means for flow separation control. AIAA J. 28 (6), 989–994. [37] Kaltenbach, H. & Janke, G. 2000 Direct numerical simulation of flow separation behind a swept rearward-facing step at Reh = 3000. Phys. Fluids 12, 2320–2337. [38] Kalter, M. -H. 2001 The reduction and elimination of a closed separation region by free-stream turbulence.
70] Zhou, M. -H. & Dengel, P. 1990 Experimental research on active separation control for lift augmentation and drag reduction. Data rep. HFI Inst. Rep. 01/90. Technische Universität Berlin. [71] Zhou, M. , Ma, H. , Wu, J. Z. & Wu, J. M. 1993 Vortex capture by a two-dimensional airfoil with a small oscillating leading-edge flap. AIAA Paper 93–3266 . [72] Zhou, M. , Kalter, M. -H. 1999 The influence of periodoc forcing on a laminar airfoil with two slots. Data rep. Technische Universität Berlin. Aerodynamic Flow Control Using Synthetic Jet Actuators Michael Amitay1 and Ari Glezer2 1 2 Aerospace, Transportation and Advanced Systems Laboratory Woodruff School of Mechanical Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0405 Abstract.