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Nathan Webb
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Cited by
Year
Control of oblique shock wave/boundary layer interactions using plasma actuators
N Webb, C Clifford, M Samimy
Experiments in fluids 54, 1-13, 2013
1392013
Excitation of free shear-layer instabilities for high-speed flow control
M Samimy, N Webb, M Crawley
AIAA journal 56 (5), 1770-1791, 2018
682018
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
592018
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
572009
Control of supersonic cavity flow using plasma actuators
N Webb, M Samimy
AIAA Journal 55 (10), 3346-3355, 2017
472017
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
412019
Coupling modes in supersonic twin rectangular jets
A Ghassemi Isfahani, NJ Webb, M Samimy
AIAA Scitech 2021 Forum, 1292, 2021
292021
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
262023
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
252013
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
202011
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
192018
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
172019
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
132022
Control of coupling in twin rectangular supersonic jets
A Ghassemi Isfahani, NJ Webb, M Samimy
AIAA Aviation 2021 Forum, 2122, 2021
132021
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
112017
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
102022
Control of flow and acoustics in twin rectangular jets
AG Isfahani, NJ Webb, M Samimy
AIAA Paper 1292, 2021, 2021
102021
Towards large-eddy simulations of supersonic jets from twin rectangular nozzle with plasma actuation
GA Bres, B Yeung, OT Schmidt, A Ghassemi Isfahani, NJ Webb, ...
AIAA AVIATION 2021 FORUM, 2154, 2021
92021
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
92019
Empirical closure model for coupling mode prediction in supersonic rectangular twin jets
N Webb, A Esfahani, S Yoder, R Leahy, M Samimy
AIAA Journal 61 (3), 1238-1247, 2023
82023
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