| Closed-loop stall control system J Poggie, CP Tilmann, PM Flick, JS Silkey, BA Osbourne, G Ervin, D Maric, ... Journal of Aircraft 47 (5), 1747-1755, 2010 | 27 | 2010 |
| Relationship of roll and pitch oscillations in a fin flapping at transitional to high Reynolds numbers PR Bandyopadhyay, DN Beal, JD Hrubes, A Mangalam Journal of fluid mechanics 702, 298-331, 2012 | 26 | 2012 |
| Closed-loop stall control on a morphing airfoil using hot-film sensors and DBD actuators J Poggie, C Tilmann, P Flick, J Silkey, B Osborne, G Ervin, D Maric, ... 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 26 | 2010 |
| Unsteady aerodynamic observables for gust load alleviation A Mangalam, S Mangalam, P Flick 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2008 | 25 | 2008 |
| Real-time unsteady loads measurements using hot-film sensors A Mangalam, T Moes 22nd Applied Aerodynamics Conference and Exhibit, 5371, 2004 | 23 | 2004 |
| Fly-by-feel sensing and control: Aeroservoelasticity AS Mangalam, MJ Brenner AIAA Atmospheric Flight Mechanics Conference, 2189, 2014 | 21 | 2014 |
| System and method for control of aeroelasticity effects AS Mangalam, SM Mangalam US Patent 8,155,794, 2012 | 21 | 2012 |
| Control of a nonlinear wing section using fly-by-feel sensing VS Suryakumar, Y Babbar, TW Strganac, AS Mangalam AIAA Atmospheric Flight Mechanics Conference, 2239, 2015 | 17 | 2015 |
| Method for predicting flow and performance characteristics of a body using critical point location SM Mangalam, A Mangalam US Patent 8,306,800, 2012 | 16 | 2012 |
| Unsteady aerodynamic model based on the leading-edge stagnation point VS Suryakumar, Y Babbar, TW Strganac, AS Mangalam Journal of Aircraft 53 (6), 1626-1637, 2016 | 13 | 2016 |
| Temperature-compensating sensor system AS Mangalam, SM Mangalam US Patent 7,653,503, 2010 | 13 | 2010 |
| Measurement and modeling of aeroelastic response under gust Y Babbar, VS Suryakumar, TW Strganac, AS Mangalam 33rd AIAA Applied Aerodynamics Conference, 2724, 2015 | 10 | 2015 |
| Formation of a proto-quasar from accretion flows in a halo A Mangalam Astronomy & Astrophysics 379 (3), 1138-1152, 2001 | 10 | 2001 |
| Flutter Suppression of an Aeroelastic Wing Using Aerodynamic Observables, Leading-Edge, and Trailing-Edge Control Surfaces J Oremland, VS Suryakumar, TW Strganac, AS Mangalam AIAA Atmospheric Flight Mechanics Conference, 4354, 2017 | 7 | 2017 |
| Models of flux tubes from constrained relaxation A Mangalam, V Krishans Journal of Astrophysics and Astronomy 21, 299-302, 2000 | 7 | 2000 |
| An Approach for Prescribed Experiments for Aerodynamic-Structural Dynamic Interaction Y Babbar, VS Suryakumar, A Mangalam, TW Strganac American Institute of Aeronautics and Astronautics, AIAA-2013-0056, 2013 | 6 | 2013 |
| A load-based feedback approach for distributed aeroservoelastic control VS Suryakumar, AS Mangalam, Y Babbar, TW Strganac AIAA Atmospheric Flight Mechanics Conference, 3101, 2016 | 5 | 2016 |
| Method and System for Determining Aerodynamic Loads from Leading Edge Flow Parameters A Mangalam US Patent App. 13/076,901, 2011 | 5 | 2011 |
| Real-time aerodynamic observable for wind turbine applications A Mangalam, G Moore, D Berg, M Blaylock, M Rumsey 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2010 | 4 | 2010 |
| Physics of supermassive disks: Formation and collapse A Mangalam arXiv preprint astro-ph/0308227, 2003 | 4 | 2003 |
