[1] Roth, J., Sherman, D., and Wilkinson, S., “Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma”, In 36th AIAA Aerospace Sciences Meeting and Exhibit, pp. 328-356, Reno, NV, U.S.A, (1998).
[2] Riherd, M., and Roy, S., “Measurements and Simulations of a Channel Flow Powered by Plasma Actuators”, Journal of Applied Physics, Vol. 112, No. 5, pp. 1-10, (2012).
[3] Enloe, C.L., McLaughlin, T.E., Van Dyken, R.D., Kachner, K.D., Jumper, E.J., and Corke, T.C., “Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology”, AIAA Journal, Vol. 42, No. 3, pp. 589-594, (2004).
[4] Pouryoussefi, S. G., and Mirzaei, M., “Experimental Study of the Unsteady Actuation Effect on Induced Flow Characteristics in DBD Plasma Actuators”, Plasma Science and Technology, Vol. 17, No. 5, pp. 415-424, (2015).
[5] Wang, C.C., and Roy, S., “Active Cooling of Turbine Blades using Horse-shoe Plasma Actuator”, In 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, pp. 679-694, (2009).
[6] Salmasi, A., Shadaram, A., Mirzaei, M., and Shams, T. A., “Numerical and Experimental Investigation on the Effect of a Plasma Actuator on NLF0414 Airfoils Efficiency after the Stall”, Modares Mechanical Engineering, Vol. 12, No. 6, pp. 104-116, (2013).
[7] Rafi, A., Amanifard, N., Deylami, H.M., and Dolati, F., “Numerical Investigation of the Plasma Actuator Effects on the Flow Field and Heat Transfer Coefficient in a Flat Channel”, Modares Mechanical Engineering, Vol. 15, No. 6, pp. 23-30, (2015).
[8] Jukes, T.N., and Choi, K.S., “Control of Unsteady Flow Separation over a Circular Cylinder using Dielectric-barrier-Discharge Surface Plasma”, Physics of Fluids, Vol. 21, No. 9, pp. 1-16, (2009).
[9] Huang, J., Corke, T.C., and Thomas, F.O., “Plasma Actuators for Separation Control of Low-pressure Turbine Blades”, AIAA Journal, Vol. 44, No. 1, pp. 51-57, (2006).
[10] De Giorgi, M.G., Ficarella, A., Marra, F., and Pescini, E., “Micro DBD Plasma Actuators for Flow Separation Control on a Low Pressure Turbine at High Altitude Flight Operating Conditions of Aircraft Engines”, Applied Thermal Engineering, Vol. 114, pp. 511-522, (2017).
[11] Roth, J.R., Sherman, D.M., and Wilkinson, S.P., “Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma”, AIAA Journal, Vol. 38, No. 7, pp. 1166-1172, (2000).
[12] Shyy, W., Jayaraman, B., and Andersson, A., “Modeling of Glow Discharge-induced Fluid Dynamics”, Journal of Applied Physics, Vol. 92, No. 11, pp. 6434-6443, (2002).
[13] Orlov, D., Corke, T., and Patel, M., “Electric Circuit Model for Aerodynamic Plasma Actuator”, In 44th AIAA Aerospace Sciences Meeting and Exhibit, pp. 1206-1216, Reno, NV, U.S.A, (2006).
[14] Suzen, Y., Huang, G., Jacob, J., and Ashpis, D., “Numerical Simulations of Plasma Based Flow Control Applications”, In 35th AIAA Fluid Dynamics Conference and Exhibit, pp. 4633-4644, Toronto, Ontario, Canada (2005).
[15] Herrig, L.J., Emery, J.C., and Erwin, J.R., “Systematic Two-dimensional Cascade Tests of NACA 65-Series Compressor Blades at Low Speeds”, NACA Technical Report 1368, (1957).
[16] Berbente, C., Andrei, I.C., Ene, N.M., Frunzulica, F., and Korody, E., “Special Topics on Map Meshing in Turbomachinery”, Periodica Polytechnica Transportation Engineering, Vol. 34, No. 1-2, pp. 59-68, (2006).
[17] Li, Y.H., Wu, Y., Zhou, M., Su, C.B., Zhang, X.W., and Zhu, J.Q., “Control of the Corner Separation in a Compressor Cascade by Steady and Unsteady Plasma Aerodynamic Actuation”, Experiments in Fluids, Vol. 48, No. 6, pp. 1015-1023, (2010).
[18] Hall, C., and Dixon, S.L., “Fluid Mechanics and Thermodynamics of Turbomachinery”, 7th Eddition, Butterworth-Heinemann, Waltham, (2013).
[19] Debiasi, M., and Li, J.M., “Experimental Study of a DBD-Plasma Driven Channel Flow”, In 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, pp. 954-967, (2011).
[20] Medic, G., Zhang, V., Wang, G., Joo, J., and Sharma, O.P., “Prediction of Transition and Losses in Compressor Cascades using Large-eddy Simulation”, Journal of Turbomachinery, Vol. 138, No. 12, pp. 1-9, (2016).
[21] Bouchmal, A., “Modeling of Dielectric-barrier Discharge Actuator”, Master of Science Thesis, Department of Aerodynamics, Delft University of Technology, Netherlands, (2011).