Iranian Journal of Mechanical Engineering Transactions of ISME

Iranian Journal of Mechanical Engineering Transactions of ISME

Numerical investigation of flow separation control in an axial compressor cascade by plasma actuation

Authors
1 University of Guilan, Faculty of engineering
2 University of Guilan, Faculty of engineering, East of Guilan
Abstract
Interest in plasma actuator as an active flow control has grown rapidly in the last years. Plasma actuator consists of a pair of electrodes that are separated by a dielectric material. Applying voltage to the electrodes, results in a body force that act on the flow field and is used in order to control it. Plasma actuator by imparting momentum is able to tangentially accelerate the flow field that can be used for flow control purpose such as boundary layer transition control, drag reduction, lift enhancement, and flow separation control. This work involves the documentation and control of leading-edge separation control that occurs on an axial compressor cascade at high angle of attack. To study the effect of control technique, a 2-D numerical investigation were performed in presence of varying plasma actuator voltage and location in different flow characteristics such as stream line, pressure and lift-to-drag ratio. The results show that plasma actuator reduce energy losses and a lift-to-drag ratio enhanced of up to 18% can be obtain by using plasma actuator at 15% of the blade chord length. The control effect obtain by the plasma actuator in low Reynolds number is more effective and Increasing the applied voltage improves the performance of the compressor cascade by increasing the induced body force.
Keywords

Subjects


[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).
Volume 20, Issue 4 - Serial Number 53
Fluid Mechanics and Heat Transfer
Winter 2019
Pages 182-209

  • Receive Date 04 August 2018
  • Revise Date 17 October 2018
  • Accept Date 12 March 2019