| Plasma flaps and slats: an application of weakly ionized plasma actuators C He, TC Corke, MP Patel Journal of aircraft 46 (3), 864-873, 2009 | 376 | 2009 |
| Plasma actuators for hingeless aerodynamic control of an unmanned air vehicle MP Patel, TT Ng, S Vasudevan, TC Corke, C He Journal of Aircraft 44 (4), 1264-1274, 2007 | 192 | 2007 |
| Scaling effects of an aerodynamic plasma actuator MP Patel, TT Ng, S Vasudevan, TC Corke, ML Post, TE McLaughlin, ... Journal of aircraft 45 (1), 223-236, 2008 | 182 | 2008 |
| Electric circuit model for aerodynamic plasma actuator D Orlov, T Corke, M Patel 44th AIAA Aerospace Sciences Meeting and Exhibit, 1206, 2006 | 178 | 2006 |
| Plasma flow control optimized airfoil T Corke, B Mertz, M Patel 44th AIAA Aerospace Sciences Meeting and Exhibit, 1208, 2006 | 148 | 2006 |
| Autonomous sensing and control of wing stall using a smart plasma slat MP Patel, ZH Sowle, TC Corke, C He Journal of aircraft 44 (2), 516-527, 2007 | 131 | 2007 |
| Flow control device and method of controlling flow FJ Lisy, M Modarreszadah, MP Patel, JM Dicocco, R Carver, RN Schmidt, ... US Patent 6,837,465, 2005 | 95 | 2005 |
| A smart wind turbine blade using distributed plasma actuators for improved performance R Nelson, T Corke, H Othman, M Patel, S Vasudevan, T Ng 46th AIAA Aerospace Sciences Meeting and Exhibit, 1312, 2008 | 87 | 2008 |
| Numerical and experimental analysis of plasma flow control over a hump model C He, T Corke, M Patel 45th AIAA aerospace sciences meeting and exhibit, 935, 2007 | 79 | 2007 |
| Modification of the flow structure over a UAV wing for roll control R Nelson, T Corke, C He, H Othman, T Matsuno, M Patel, T Ng 45th AIAA aerospace sciences meeting and exhibit, 884, 2007 | 57 | 2007 |
| Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators M Patel, T Corke US Patent 7,624,941, 2009 | 50 | 2009 |
| Aircraft and missile afterbody flow control device and method of controlling flow J DiCocco, T Prince, M Patel, TMT Ng US Patent 7,070,144, 2006 | 50 | 2006 |
| Aircraft and missile forebody flow control device and method of controlling flow T Prince, FJ Lisy, MP Patel, JM DiCocco, R Carver, RN Schmidt US Patent 6,685,143, 2004 | 44 | 2004 |
| Mechanism of vorticity generation in plasma streamwise vortex generators M Wicks, FO Thomas, TC Corke, M Patel, AB Cain AIAA Journal 53 (11), 3404-3413, 2015 | 41 | 2015 |
| Aerodynamic control of using windward-surface plasma actuators on a separation ramp J Lopera, TT Ng, MP Patel, S Vasudevan, E Santavicca, TC Corke Journal of Aircraft 44 (6), 1889-1895, 2007 | 40 | 2007 |
| GreenFire energy closed-loop geothermal demonstration using supercritical carbon dioxide as working fluid A Amaya, J Scherer, J Muir, M Patel, B Higgins Proceedings of the 45th Workshop on Geothermal Reservoir Engineering …, 2020 | 37 | 2020 |
| Closed-loop missile yaw control via manipulation of forebody flow asymmetrics MP Patel, CP Tilmann, TT Ng Journal of Spacecraft and Rockets 41 (3), 436-443, 2004 | 34 | 2004 |
| A parametric investigation of plasma streamwise vortex generator performance M Wicks, F Thomas, D Schatzman, P Bowles, T Corke, M Patel, A Cain 50th AIAA aerospace sciences meeting including the new horizons forum and …, 2012 | 29 | 2012 |
| Reconfigurable porous technology for fluid flow control and method of controlling flow MP Patel, JM Dicocco, T Prince US Patent 6,866,233, 2005 | 27 | 2005 |
| Hierarchical closed-loop control system for aircraft, missiles and munitions TS Prince, R Kolacinski, M Patel US Patent 8,190,305, 2012 | 26 | 2012 |
