| Reattachment streaks in hypersonic compression ramp flow: an input–output analysis A Dwivedi, GS Sidharth, JW Nichols, GV Candler, MR Jovanović Journal of Fluid Mechanics 880, 113-135, 2019 | 104 | 2019 |
| Simulation and stability analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92 N Hildebrand, A Dwivedi, JW Nichols, MR Jovanović, GV Candler Physical Review Fluids 3 (1), 013906, 2018 | 79 | 2018 |
| Onset of three-dimensionality in supersonic flow over a slender double wedge S Gs, A Dwivedi, GV Candler, JW Nichols Physical Review Fluids 3 (9), 093901, 2018 | 65 | 2018 |
| Direct numerical simulation of BOLT hypersonic flight vehicle J Thome, A Dwivedi, JW Nichols, GV Candler 2018 Fluid Dynamics Conference, 2894, 2018 | 46 | 2018 |
| Input-output analysis of shock boundary layer interaction A Dwivedi, S Gs, GV Candler, JW Nichols, M Jovanovic 2018 Fluid Dynamics Conference, 3220, 2018 | 38 | 2018 |
| Oblique transition in hypersonic double-wedge flow A Dwivedi, GS Sidharth, MR Jovanović Journal of Fluid Mechanics 948, A37, 2022 | 29 | 2022 |
| Global linear stability analysis of high speed flows on compression ramps S Gs, A Dwivedi, GV Candler, JW Nichols 47th AIAA Fluid Dynamics Conference, 3455, 2017 | 23 | 2017 |
| Optimal spatial growth of streaks in oblique shock/boundary layer interaction A Dwivedi, JW Nichols, MR Jovanovic, GV Candler 8th AIAA Theoretical Fluid Mechanics Conference, 4163, 2017 | 21 | 2017 |
| Computational study of flow on a sliced cone-flap geometry J Thome, JD Reinert, A Dwivedi, GV Candler 2018 Fluid Dynamics Conference, 3397, 2018 | 18 | 2018 |
| Interaction of an oblique shock with a transitional Mach 5.92 boundary layer P Shrestha, NJ Hildebrand, A Dwivedi, JW Nichols, MR Jovanovic, ... 46th AIAA Fluid Dynamics Conference, 3647, 2016 | 17 | 2016 |
| Transient growth analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92 A Dwivedi, N Hildebrand, JW Nichols, GV Candler, MR Jovanović Physical Review Fluids 5 (6), 063904, 2020 | 14 | 2020 |
| Verification of a conjugate heat transfer tool with US3D JD Reinert, A Dwivedi, GV Candler AIAA Scitech 2019 Forum, 1892, 2019 | 14 | 2019 |
| Three-dimensionality in shock/boundary layer interactions: a numerical and experimental investigation A Dwivedi, CJ Broslawski, GV Candler, RD Bowersox AIAA AVIATION 2020 FORUM, 3011, 2020 | 11 | 2020 |
| Nose Bluntness Effects on the Amplification of External Disturbances in Hypersonic Flows L Melander, A Dwivedi, GV Candler AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 …, 2022 | 8 | 2022 |
| Numerical investigation of nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow LJ Melander, A Dwivedi, GV Candler AIAA Scitech 2022 Forum, 0948, 2022 | 7 | 2022 |
| Global input-output analysis of flow instabilities in high-speed compressible flows A Dwivedi University of Minnesota, 2020 | 7 | 2020 |
| Görtler instability analysis of Mach 6 flow on a flared axisymmetric cone with and without suction C Hollender, A Dwivedi, GV Candler AIAA Aviation 2019 Forum, 3219, 2019 | 5 | 2019 |
| A frequency domain analysis of compressible linearized Navier-Stokes equations in a hypersonic compression ramp flow A Dwivedi, GV Candler, MR Jovanović 2020 American Control Conference (ACC), 4325-4330, 2020 | 3 | 2020 |
| Input-output analysis for Görtler-type instability in axisymmetric hypersonic boundary-layers A Dwivedi, S Gs, C Hollender, GV Candler AIAA AVIATION 2020 FORUM, 2987, 2020 | 3 | 2020 |
| Local and biglobal linear stability analysis of parallel shear flows S Mittal, A Dwivedi Computer Modeling in Engineering & Sciences 113 (2), 219-237, 2017 | 3 | 2017 |
Graham V. CandlerRussell J. Penrose and McKnight Presidential Professor of Aerospace Engineering & MechanicsVerified email at umn.edu
