| Suppression of cavity flow oscillations via three-dimensional steady blowing Y Zhang, Y Sun, N Arora, LN Cattafesta III, K Taira, LS Ukeiley AIAA journal 57 (1), 90-105, 2019 | 47 | 2019 |
| Flowfield of a 3-D swept shock boundary layer interaction in a Mach 2 flow N Arora, MY Ali, FS Alvi 46th AIAA fluid dynamics conference, 3649, 2016 | 32 | 2016 |
| Unsteady characteristics of a swept-shock/boundary-layer interaction at Mach 2 N Arora, L Mears, FS Alvi AIAA Journal 57 (10), 4548-4559, 2019 | 30 | 2019 |
| Flowfield measurements in a Mach 2 fin-generated shock/boundary-layer interaction N Arora, MY Ali, Y Zhang, FS Alvi AIAA Journal 56 (10), 3963-3974, 2018 | 29 | 2018 |
| Introducing controlled perturbations in a 3-D swept shock boundary layer interaction L Mears, N Arora, FS Alvi 2018 AIAA Aerospace Sciences Meeting, 2076, 2018 | 26 | 2018 |
| Effect of Reynolds number on 3-D shock wave boundary layer interactions AK Baldwin, N Arora, R Kumar, FS Alvi 46th AIAA Fluid Dynamics Conference, 3339, 2016 | 19 | 2016 |
| Skin friction measurements using oil film interferometry in a 3-d supersonic flowfield A Baldwin, LJ Mears, N Arora, R Kumar, FS Alvi, JW Naughton AIAA Journal 57 (4), 1373-1382, 2019 | 17 | 2019 |
| Flowfield response to controlled perturbations in swept shock/boundary-layer interaction using unsteady PSP L Mears, N Arora, FS Alvi AIAA Scitech 2019 forum, 0094, 2019 | 17 | 2019 |
| Shock-boundary layer interaction due to a sharp unswept fin in a Mach 2 flow N Arora, MY Ali, Y Zhang, FS Alvi 53rd AIAA aerospace sciences meeting, 1517, 2015 | 16 | 2015 |
| Single-camera three-dimensional velocity measurement of a fin-generated shock-wave/boundary-layer interaction C Jones, J Bolton, C Clifford, B Thurow, N Arora, F Alvi AIAA Journal 58 (10), 4438-4450, 2020 | 13 | 2020 |
| Single camera 3D measurement of a shock wave-turbulent boundary layer interaction JT Bolton, BS Thurow, FS Alvi, N Arora 55th AIAA Aerospace Sciences Meeting, 0985, 2017 | 11 | 2017 |
| Volumetric measurement of a shock wave-turbulent boundary layer interaction using plenoptic particle image velocimetry JT Bolton, BS Thurow, FS Alvi, N Arora 32nd AIAA aerodynamic measurement technology and ground testing conference, 4029, 2016 | 11 | 2016 |
| Visualization of an SBLI using Plenoptic BOS CJ Clifford, JN Klemkowsky, BS Thurow, N Arora, FS Alvi 55th AIAA Aerospace Sciences Meeting, 1643, 2017 | 9 | 2017 |
| Properties of resonance enhanced microjets in supersonic crossflow MY Ali, N Arora, M Topolski, FS Alvi, JT Solomon AIAA Journal 55 (3), 1075-1081, 2017 | 7 | 2017 |
| Preliminary plenoptic PIV results for volumetric measurements of shock wave-boundary layer interactions C Jones, C Clifford, JT Bolton, BS Thurow, L Mears, FS Alvi 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 4065, 2017 | 7 | 2017 |
| Three-dimensional flowfield of microjets in supersonic crossflow MY Ali, N Arora, FS Alvi 43rd AIAA Fluid Dynamics Conference, 3117, 2013 | 7 | 2013 |
| Flowfield of a three-dimensional swept-shock boundary layer interaction at Mach 2 N Arora The Florida State University, 2018 | 5 | 2018 |
| Experiments on Resonance Enhanced Pulsed Microjet Actuators in Supersonic Crossflow M Topolski, N Arora, M Ali, J Solomon, F Alvi 6th AIAA Flow Control Conference, 2813, 2012 | 5 | 2012 |
| Two camera plenoptic PIV applied to shock wave-boundary layer interactions C Jones, C Clifford, BS Thurow, L Mears, N Arora, FS Alvi 2018 Fluid Dynamics Conference, 3705, 2018 | 3 | 2018 |
| Oil Film Interferometry on the Surface Under a Three-Dimensional Flow Field A Baldwin, N Arora, L Mears, R Kumar, FS Alvi, JW Naughton 2018 AIAA Aerospace Sciences Meeting, 0300, 2018 | 3 | 2018 |
Farrukh AlviProf of Mech. Engineering; Assoc. Provost - Innovation, Research & Entrepreneurship, Fl State Univ.Verified email at fsu.edu
