Gad-el Hak, M., Flow Control: Passive, Active, Reactive Flow Management, Cambridge University Press, New York, 2000.
	Greenblatt, D. and Wygnanski, I., The control of flow separation by periodic excitation, Progress in Aerospace Sciences, Vol. 36, No. 7, 2000, pp. 487-545. CrossRef
	McLean, J. D., Crouch, J. D., Stoner, R. C., Sakurai, S., Seidel, G. E., Feifel, W. M., and Rush, H. M., Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft, NASA/CR-1999-209338, 1999.
	Rudolph, P. K. C., High-Lift Systems on Commercial Subsonic Airliners, NASA CR 4746, Sept. 1996.
	Hassan, A. A., Improving Flap Aerodynamics Using Oscillatory Jet Control, AIAA Paper 2003-3664.
	Kiedaisch J., Nagib, H., and Demanett, B., Active Flow Control Applied to High-Lift Airfoils Utilizing Simple Flaps, AIAA Paper 2006-2856, 2006.
	Meunier, M., Simulation and Optimization of Flow Control Strategies for Novel High-Lift Configurations, AIAA Journal, Vol. 47, No. 5, 2009, pp. 1145-1157. CrossRef
	Crowther, W. J., Separation Control on a Trailing-Edge Flap Using Air Jet Vortex Generators, Journal of Aircraft, Vol. 43, No. 5, 2006, 1589-1593. CrossRef
	Khodadoust A., Washburn A, Active Control of Flow Separation on a High-Lift System with Slotted Flap at High Reynolds Number, AIAA Paper 2007-4424, 2007.
	Shmilovich, A. and Yadlin, Y., Active flow control for practical high-lift systems, Journal of Aircraft, Vol. 46, No. 4, 2009, pp.1354-1364. CrossRef
	Petz, R. and Nitsche W., Active Separation Control on the Flap of a Two-Dimensional Generic High-Lift Configuration, Journal of Aircraft, Vol. 44, No. 3, 2007, pp. 865-874. CrossRef
	Wild, J., Wichmann, G., Haucke, F., Peltzer, I. and Scholz, P., Large scale separation flow control experiments within the German Flow Control Network, AIAA Paper 2009-530, Jan. 2009.
	Haucke, F. and Nitsche, W., Active Flow Control on the Flap of a 2D High-Lift Wing Section at Re = 1 x 106, AIAA Paper 2011-3359, June 2011.
	Ciobaca, V., Parameter study for a slatless 2D high-lift airfoil with active separation control using a URANS approach, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 121, pp. 135-142, 2012.
	Joslin, R. D., Miller, D. N., Fundamentals and Applications of Modern Active Flow Control, AIAA Book, Progress in Astronautics and Aeronautics, vol. 231, ISBN 978-1-56347-983-0, 2009.
	Wild, J., Experimental investigations of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections, AIAA Paper 2012-108, 2012.
	http://www.cleansky.eu/
	Poisson-Quinton, Ph., Recherches théoriques et expérimentales sur le contrôle de couche limite, 7th Congress of Applied Mechanics, London, September 1948.
	http://centaursoft.com
	Cambier, L. and Gazaix, M., elsA: an Efficient Object-Oriented Solution to CFD Complexity, AIAA 2002-0108, 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno (NV), January 14-17, 2002. http://elsa.onera.fr/ http://elsa.onera.fr/
	Cambier, L. and Veuillot, J.-P., Status of the elsA CFD Software for Flow Simulation and Multidisciplinary Applications, AIAA 2008-0664, Jan. 2008.
	Spalart, P. and Allmaras, S., A One Equation Turbulence Model for Aerodynamic Flows, La Recherche Aérospatiale, 1994, Pages 5-21.
	Gerhold, T.: Overview of the Hybrid RANS Code TAU, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 89, Springer Verlag, pp. 81-92, 2005.
	Menter, F. R., Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications, AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605. CrossRef
	Rudnik, R., Evaluation of the Performance of Two-Equation Turbulence Models for Airfoil Flows, Ph.D. Dissertation, Transportation and Applied Mechanics Dept., Technical University Berlin, Germany, 1997.
	Moens, F., Perraud, J., Séraudie, A. and Houdeville, R., Transition Measurement and Prediction on a Generic High-Lift Swept Wing, Proceedings of the Institution of Mechanical Engineers, Part G (Journal of Aerospace Engineering), Vol. 220, pp. 589-603, June 2006.
	Krumbein, A., Krimmelbein, N. and Schrauf G., Automatic transition prediction in a hybrid flow solver, part 1: Methodology and sensitivities, Journal of Aircraft, Vol. 46, No. 4, pp. 1176-1190, 2006. CrossRef
	Krumbein, A., Krimmelbein, N. and Seyfert, C., Automatic transition prediction in unsteady airfoil flows using an unstructured CFD code, AIAA Paper 2011-3365, 2011.
	Knopp, T., The actuation boundary condition for flow control in the DLR TAU Code, DLR Report, IB-Nr. 224 - 2010 A44, Germany, 2010.
	Togiti, V., Ciobaca, V., Eisfeld, B. and Knopp T., Numerical Simulation of Steady Blowing Active Flow Control Using a Differential Reynolds Stress Model, Proceedings of CEAS/KATnet II Conference on Key Aerodynamics Technologies, Bremen, Germany, May 2009.
	Schlichting, H. and Truckenbrodt, E., Aerodynamics of the Airplane, McGraw-Hill, 1979.