| Secondary flow structures due to interaction between a finite-span synthetic jet and a 3-D cross flow Y Elimelech, J Vasile, M Amitay Physics of Fluids 23 (9), 2011 | 36 | 2011 |
| Active control of inlet ducts J Vaccaro, M Amitay, J Vasile 26th AIAA Applied Aerodynamics Conference, 6402, 2008 | 35 | 2008 |
| Aerodynamic design optimization of long range projectiles using missile DATCOM JD Vasile, J Bryson, F Fresconi AIAA Scitech 2020 Forum, 1762, 2020 | 28 | 2020 |
| Interactions of an array of finite span synthetic jets and a crossflow JD Vasile, M Amitay AIAA journal 51 (10), 2503-2512, 2013 | 23 | 2013 |
| A multi-disciplinary approach to design long range guided projectiles JD Vasile, J Bryson, BC Gruenwald, L Fairfax, L Strohm, F Fresconi AIAA Scitech 2020 Forum, 1993, 2020 | 15 | 2020 |
| Aerodynamic Dataset Generation of a Long-Range Projectile JD Vasile, JT Bryson, J Sahu, JL Paul, BC Gruenwald CCDC Army Research Lab. TR-9019, Aberdeen Proving Ground, 2020 | 14 | 2020 |
| Roll Orientation-Dependent Aerodynamics of a Long Range Projectile JD Vasile, J Sahu AIAA Scitech 2021 Forum, 0023, 2021 | 12 | 2021 |
| Approach for understanding range extension of gliding indirect fire munitions J Bryson, JD Vasile, I Celmins, F Fresconi 2018 Atmospheric Flight Mechanics Conference, 3158, 2018 | 12 | 2018 |
| Interaction of a finite-span synthetic jet near the tip of a sweptback wing JD Vasile, M Amitay Physics of Fluids 27 (6), 2015 | 12 | 2015 |
| Control surface design analysis and actuation requirements development for munitions J Bryson, JD Vasile, BC Gruenwald, F Fresconi AIAA Scitech 2020 Forum, 0020, 2020 | 11 | 2020 |
| Combining sparse and dense databases to form a robust aerodynamic model for a long-range, high-speed projectile BT Burchett, JD Vasile, J Bryson AIAA Scitech 2022 Forum, 0419, 2022 | 9 | 2022 |
| Modeling and flight dynamics of a projectile with nonlinear, roll-dependent aerodynamics J Bryson, JD Vasile, BC Gruenwald, J Saju, F Fresconi AIAA Scitech 2021 Forum, 0823, 2021 | 9 | 2021 |
| Experimental and computational aerodynamic characterization of a generic high-speed projectile configuration RC Pokela, R Kumar, JD Vasile AIAA Aviation 2021 Forum, 2607, 2021 | 8 | 2021 |
| A High Fidelity Roll Dependent Aerodynamic Model for a Long Range, High Speed Missile BT Burchett, JL Paul, JD Vasile, J Bryson AIAA Scitech 2022 Forum, 0420, 2022 | 7 | 2022 |
| Trajectory shaping for quasi-equilibrium glide in guided munitions LD Fairfax, JD Vasile, L Strohm, F Fresconi AIAA Scitech 2020 Forum, 0021, 2020 | 7 | 2020 |
| Interaction of a finite-span synthetic-jet and a cross-flow over a sweptback finite wing J Vasile, M Amitay 6th AIAA Flow Control Conference, 2948, 2012 | 7 | 2012 |
| Aerodynamic dataset generation of a long range projectile. DEVCOM Army Research Laboratory (US); 2020 Aug. Report No J Vasile, J Bryson, J Sahu, J Paul, B Gruenwald ARL-TR-9019, 0 | 7 | |
| Roll orientation-dependent aerodynamics of a long-range projectile. DEVCOM Army Research Laboratory (US); 2020 Aug. Report No JD Vasile, J Sahu ARL-TR-9017, 0 | 6 | |
| High-speed army reference vehicle JD Vasile, F Fresconi, J DeSpirito, M Duca, T Recchia, B Grantham, ... US Army Combat Capabilities Development Command, Army Research Laboratory, 2022 | 5 | 2022 |
| Aerodynamic design optimization of control mechanisms for a subsonic, small diameter munition JD Vasile, F Fresconi, I Celmins, B Nelson 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2018 | 5 | 2018 |
Joshua T. BrysonUS Army Research LabVerified email at mail.mil
