Mechanism of flow separation control using plasma actuation
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[1] F. Browand,et al. Vortex pairing : the mechanism of turbulent mixing-layer growth at moderate Reynolds number , 1974, Journal of Fluid Mechanics.
[2] Chih-Ming Ho,et al. Subharmonics and vortex merging in mixing layers , 1982, Journal of Fluid Mechanics.
[3] B. Nishri,et al. Effects of Periodic Excitation on Turbulent Flow Separation from a Flap , 1998 .
[4] Chih-Ming Ho,et al. Perturbed Free Shear Layers , 1984 .
[5] Israel J Wygnanski,et al. Active management of naturally separated flow over a solid surface. Part 1. The forced reattachment process , 2004, Journal of Fluid Mechanics.
[6] A. Roshko,et al. On density effects and large structure in turbulent mixing layers , 1974, Journal of Fluid Mechanics.
[7] Thomas McLaughlin,et al. Parameterization of Temporal Structure in the Single Dielectric Barrier Aerodynamic Plasma Actuator , 2006 .
[8] Christopher L. Rumsey,et al. Summary of the 2004 Computational Fluid Dynamics Validation Workshop on Synthetic Jets , 2006 .
[9] Ari Glezer,et al. Evolution of stream wise vortices and generation of small-scale motion in a plane mixing layer , 1991, Journal of Fluid Mechanics.
[10] Subcritical Pipe Flow Transition Control Using Dielectric Barrier Discharge Plasma Actuators , 2009 .
[11] Yannick Hoarau,et al. Organized modes and the three-dimensional transition to turbulence in the incompressible flow around a NACA0012 wing , 2003, Journal of Fluid Mechanics.
[12] Keith B. Paschal,et al. Experimental Investigation of Separation Control Part 2: Zero Mass-Flux Oscillatory Blowing , 2006 .
[13] I. Wygnanski,et al. On the periodically excited plane turbulent mixing layer, emanating from a jagged partition , 2007, Journal of Fluid Mechanics.
[14] Peter A. Monkewitz,et al. Influence of the velocity ratio on the spatial instability of mixing layers , 1982 .
[15] Israel J Wygnanski,et al. Active management of naturally separated flow over a solid surface. Part 2. The separation process , 2004, Journal of Fluid Mechanics.
[16] C. O. Paschereit,et al. Plasma Flow Control on Low Aspect Ratio Wings at Low Reynolds Numbers , 2010 .
[17] Kwing-So Choi,et al. Control of unsteady flow separation over a circular cylinder using dielectric-barrier-discharge surface plasma , 2009 .
[18] Israel J Wygnanski,et al. On the effect of initial conditions on the two dimensional turbulent mixing layer , 1978 .
[19] Wei Shyy,et al. Flapping and flexible wings for biological and micro air vehicles , 1999 .
[20] C. R. Smith,et al. Vortex Interactions with Walls , 1994 .
[21] Israel J Wygnanski,et al. Effect of Leading-Edge Curvature on Airfoil Separation Control , 2003 .
[22] Jinhee Jeong,et al. On the identification of a vortex , 1995, Journal of Fluid Mechanics.
[23] Christian Oliver Paschereit,et al. Dielectric Barrier Discharge Flow Control at Very Low Flight Reynolds Numbers , 2008 .
[24] Luis P. Bernal,et al. Streamwise vortex structure in plane mixing layers , 1986, Journal of Fluid Mechanics.
[25] Andrew Ooi,et al. On the coherent structures and stability properties of a leading-edge separated aerofoil with turbulent recirculation , 2011, Journal of Fluid Mechanics.
[26] Chih-Ming Ho,et al. Unsteady aerodynamics and flow control for flapping wing flyers , 2003 .
[27] T. Corke,et al. SDBD plasma enhanced aerodynamics: concepts, optimization and applications , 2007 .
[28] Christopher L. Rumsey,et al. Prediction of high lift: review of present CFD capability , 2002 .
[29] Israel J Wygnanski,et al. The control of flow separation by periodic excitation , 2000 .
[30] T. Mueller,et al. AERODYNAMICS OF SMALL VEHICLES , 2003 .