Control of oblique shock wave/boundary layer interactions using plasma actuators N Webb, C Clifford, M Samimy Experiments in fluids 54, 1-13, 2013 | 132 | 2013 |
Excitation of free shear-layer instabilities for high-speed flow control M Samimy, N Webb, M Crawley AIAA journal 56 (5), 1770-1791, 2018 | 62 | 2018 |
Supersonic inlet flow control using plasma actuators E Caraballo, N Webb, J Little, JH Kim, M Samimy 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2009 | 55 | 2009 |
Control of dynamic stall over a NACA 0015 airfoil using plasma actuators A Singhal, D Castañeda, N Webb, M Samimy AIAA Journal 56 (1), 78-89, 2018 | 53 | 2018 |
Control of supersonic cavity flow using plasma actuators N Webb, M Samimy AIAA Journal 55 (10), 3346-3355, 2017 | 44 | 2017 |
Reinventing the wheel: excitation of flow instabilities for active flow control using plasma actuators M Samimy, N Webb, A Esfahani Journal of Physics D: Applied Physics 52 (35), 354002, 2019 | 39 | 2019 |
Coupling modes in supersonic twin rectangular jets A Ghassemi Isfahani, NJ Webb, M Samimy AIAA Scitech 2021 Forum, 1292, 2021 | 27 | 2021 |
An investigation of the control mechanism of plasma actuators in a shock wave-boundary layer interaction N Webb, C Clifford, M Samimy 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2013 | 25 | 2013 |
Preliminary results on shock wave/boundary layer interaction control using localized arc filament plasma actuators N Webb, C Clifford, M Samimy 41st AIAA Fluid Dynamics Conference and Exhibit, 3426, 2011 | 19 | 2011 |
Stall cell formation over a post-stall airfoil: effects of active perturbations using plasma actuators A Esfahani, N Webb, M Samimy Experiments in Fluids 59, 1-16, 2018 | 18 | 2018 |
Perturbation-based active flow control in overexpanded to underexpanded supersonic rectangular twin jets M Samimy, N Webb, A Esfahani, R Leahy Journal of Fluid Mechanics 959, A13, 2023 | 17 | 2023 |
Flow separation control over a thin post-stall airfoil: effects of excitation frequency A Esfahani, N Webb, M Samimy AIAA Journal 57 (5), 1826-1838, 2019 | 15 | 2019 |
Control of coupling in twin rectangular supersonic jets A Ghassemi Isfahani, NJ Webb, M Samimy AIAA Aviation 2021 Forum, 2122, 2021 | 12 | 2021 |
Unsteady flow separation control over a NACA 0015 using NS-DBD plasma actuators A Singhal, D Castañeda, NJ Webb, M Samimy 55th AIAA Aerospace Sciences Meeting, 1687, 2017 | 11 | 2017 |
An experimental investigation of deep dynamic stall control using plasma actuators D Castañeda, N Whiting, N Webb, M Samimy Experiments in Fluids 63 (4), 69, 2022 | 10 | 2022 |
Design and characterization of an experimental setup for active control of dynamic stall over a NACA 0012 airfoil D Castaneda, N Whiting, NJ Webb, M Samimy AIAA Aviation 2019 Forum, 3212, 2019 | 10 | 2019 |
Control of flow and acoustics in twin rectangular jets AG Isfahani, NJ Webb, M Samimy AIAA Paper 1292, 2021, 2021 | 9 | 2021 |
The effects of active control on near-field pressure fluctuations in supersonic rectangular twin jets RP Leahy, A Ghassemi Isfahani, NJ Webb, M Samimy 28th AIAA/CEAS Aeroacoustics 2022 Conference, 2968, 2022 | 8 | 2022 |
Control of dynamic stall over a NACA 0012 airfoil using NS-DBD plasma actuators NL Whiting, D Castaneda, NJ Webb, M Samimy AIAA Scitech 2020 Forum, 1568, 2020 | 8 | 2020 |
Supersonic cavity control using plasma actuators NJ Webb, M Samimy 53rd AIAA Aerospace Sciences Meeting, 1961, 2015 | 8 | 2015 |