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Acknowledgment This work was conducted under a SBIR Phase II Program from the USAF/AFRL, VA, under Contract No. FA8650-04-C-3405 monitored by the USAF Program Manager Charles F. Suchomel. References [1] Corke, T. C., Design of Aircraft, Prentice–Hall, New York, 2002. [2] Corke, T. C., He, C., and Patel, M. P., “Plasma Flaps and Slats: An Application of Weakly-Ionized Plasma Actuators,” AIAA Paper 2004- 2127, July 2004. [3] Chang, P. K., Control of Separation, McGraw–Hill, New York, 1976. [4] Gad-el-Hak, M., and Bushnell, D. M., “Separation Control: Review,” Journal of Fluid Engineering, Vol. 113, March 1991, pp. 5–30. [5] Greenblatt, D., and Wygnanski, I., “Control of Separation by Periodic Excitation,” Progress in Aerospace Sciences, Vol. 37, No. 7, 2000, pp. 487–545. [6] Seifert, A., Darabi, A., and Wygnanski, I., “Delay of Airfoil Stall by Periodic Excitation,” Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 691– 698. [7] Lin, J. C., Robinson, S. K., McGhee, R. J., and Valarezo, W. O., “Separation Control on High-Lift Airfoils Via Micro-Vortex Generators,” Journal of Aircraft, Vol. 31, No. 6, 1994, pp. 1317–1323. [8] Patel, M. P., Tilmann, C. P., and Ng, T. T., “Active Transparent Stall Control System for Air Vehicles,” Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 993–997. [9] McManus, K. R., Joshi, P. B., Legner, H. H., and Davis, S. J., “Active Control of Aerodynamic Stall Using Pulsed Jet Actuators,” AIAA Paper 1995-2187, June 1995. [10] Corke, T. C., and Post, M., “Overview of Plasma Flow Control: Concepts, Optimization, and Applications,” AIAA Paper 2005-0563, Jan. 2005. [11] Goradia,SureshH.,andLyman,Victor,“LaminarStallPredictionand Estimation of CLmax,” Journal of Aircraft, Vol. 11, No. 9, 1974, pp. 528–536. [12] Enloe, L., McLaughlin, T., VanDyken, R., Kachner, Jumper, E., and Corke, T. C., “Mechanisms and Response of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology,” AIAA Journal, Vol. 42, No. 3, [13] [14] [15] [16] [17] [18] [19] [20] [21] [22] [23] [24] [25] March 2004, pp. 589–594. Enloe,L.,McLaughlin,T.,VanDyken,R.,Kachner,Jumper,E.,Corke, T. C., Post, M., and Haddad, O., “Mechanisms and Response of a Single Dielectric Barrier Plasma Actuator: Geometric Effects,” AIAA Journal, Vol. 42, No. 3, March 2004, pp. 595–604. Orlov,D.M.,andCorke,T.C.,“NumericalSimulationofAerodynamic Plasma Actuator Effects,” AIAA Paper 2005-1083, Jan. 2005. Nelson,C.C.,Cain,A.B.,Patel,M.P.,andCorke,T.C.,“Simulationof Plasma Actuators Using the Wind-US Code,” AIAA Paper 2006-0634, Jan. 2006. Orlov,D.M.,Corke,T.C.,andPatel,M.P.,“ElectricCircuitModelfor the Aerodynamic Plasma Actuator,” AIAA Paper 2006-1206, Jan. 2006. Corke,T.C.,Cavalieri,D.,andMatlis,E.,“BoundaryLayerInstability on a Sharp Cone at Mach 3.5 with Controlled Input,” AIAA Journal, Vol. 40, No. 5, 2001, pp. 1015–1018. Corke, T. C., Jumper, E., Post, M., Orlov, D. and McLaughlin, T., “Application of Weakly-Ionized Plasmas as Wing Flow-Control Devices,” AIAA Paper 2002-0350, Jan. 2002. Huang, J., Corke, T. C., and Thomas, F., “Plasma Actuators for Separation Control of Low-Pressure Turbine Blades,” AIAA Paper 2003-1027, AIAA Journal (to be pubished).. Post, M., and Corke, T. C., “Separation Control on High Angle of Attack Airfoil Using Plasma Actuators,” AIAA Journal, Vol. 42, No. 11, 2004, pp. 2177–2184; also AIAA Paper 2003-1024. Corke,T.C.,andMatlis,E.,“PhasedPlasmaArraysforUnsteadyFlow Control,” AIAA Paper 2000-2323, Jan. 2000. Post,M.,andCorke,T.C.,“SeparationControlUsingPlasmaActuators —Stationary and Oscillating Airfoils,” AIAA Paper 2004-0841, 2004. Corke, T. C., Mertz, B., and Patel, M. P., “Plasma Flow Control Optimized Airfoil,” AIAA Paper 2006-1208, Jan. 2006. Patel,M.P.,Ng,T.T.,Vasudevan,S.,Corke,T.C.,andHe,C.,“Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle,” AIAA Paper 2006-3495, June 2006. Broeren, A. P., and Bragg, M. B., “Flowfield Measurements over an Airfoil During Natural Low-Frequency Oscillation near Stall,” AIAA Journal, Vol. 37, No. 1, 1999, pp. 130–132. View publication stats PATEL ET AL. 527PDF Image | Autonomous Sensing and Control of Wing Stall Using a Smart Plasma Slat
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