| Stabilized detonation for hypersonic propulsion DA Rosato, M Thornton, J Sosa, C Bachman, GB Goodwin, KA Ahmed Proceedings of the National Academy of Sciences 118 (20), 2021 | 116 | 2021 |
| Controlled detonation initiation in hypersonic flow J Sosa, DA Rosato, GB Goodwin, CL Bachman, ES Oran, KA Ahmed Proceedings of the Combustion Institute 38 (3), 3513-3520, 2021 | 13 | 2021 |
| Ignition mechanisms of pulse detonator initiated scramjet cavity DA Rosato, TM Ombrello, D Cuppoletti, CD Carter, SD Hammack, ... Proceedings of the Combustion Institute 38 (3), 3853-3860, 2021 | 13 | 2021 |
| Experimental Study of Oblique Detonation Waves with Varied Ramp Geometries MR Thornton, DA Rosato, KA Ahmed AIAA SCITECH 2022 Forum, 1753, 2022 | 5 | 2022 |
| The Propagation Characteristics of a Detonation Wave in a Supersonic Mach 5 Flow J Sosa, K Ahmed, D Rosato 2018 AIAA Aerospace Sciences Meeting, 1419, 2018 | 5 | 2018 |
| Shock-Induced High-Speed Reactions in High Enthalpy Hypersonic Flow D Rosato, J Sosa, KA Ahmed AIAA Scitech 2020 Forum, 0924, 2020 | 4 | 2020 |
| Effects of Detonation Decoupling on the Ignition of a Supersonic Cavity for Scramjets DA Rosato, KA Ahmed, DR Cuppoletti, T Ombrello, CD Carter, ... AIAA Scitech 2020 Forum, 1612, 2020 | 3 | 2020 |
| Comparison of Measured and Calculated Detonation Propagation Velocities from a Pre-Detonator in Supersonic Crossflow DA Rosato, J Sosa, KA Ahmed 2018 Joint Propulsion Conference, 4689, 2018 | 3 | 2018 |
| Fuel Distribution Measurements in a Hypersonic Combustor Facility DA Rosato, M Thornton, J Reyes, KA Ahmed AIAA Propulsion and Energy 2021 Forum, 3526, 2021 | 2 | 2021 |
| Experimental Measurements of Oblique Shock Induced Reactions in Hypersonic Wedge Flow DA Rosato, KA Ahmed AIAA Propulsion and Energy 2020 Forum, 3858, 2020 | 1 | 2020 |
| Detonation Wave Mach Number Dependence in a High Mach Number Flows J Sosa, D Rosato, K Ahmed 22nd AIAA International Space Planes and Hypersonics Systems and …, 2018 | 1 | 2018 |
| Design and Characterization of Mach 5 Flow for Highly Turbulent Hypersonic Test Facility MR Thornton, DA Rosato, KA Ahmed AIAA Scitech 2021 Forum, 0383, 2021 | | 2021 |
| Study of Oblique Shock Induced Reactions at Moderate Total Temperatures DA Rosato, M Thornton, KA Ahmed AIAA Scitech 2021 Forum, 0687, 2021 | | 2021 |
| Ignition of Supersonic Flows Via Pulse Detonator D Rosato | | 2020 |
| Auto-Ignition and Detonation of H2/Air Mixtures in Hypersonic Flows J Sosa, DA Rosato, KA Ahmed, ES Oran, CR Kaplan, GB Goodwin AIAA Scitech 2019 Forum, 1256, 2019 | | 2019 |
| Mach Number Effect on Propagation and Stabilization of Detonation Waves DA Rosato, J Sosa, KA Ahmed AIAA Scitech 2019 Forum, 0749, 2019 | | 2019 |
| Characteristics of Hypersonic Mach 5 Turbulent Reacting Flow D Rosato, J Sosa, K Ahmed Bulletin of the American Physical Society 63, 2018 | | 2018 |
| Initiation of Sustained Reaction in Premixed, Combustible Supersonic Flow Via a Predetonator DA Rosato | | 2018 |
| PROPAGATION OF A DETONATION WAVE IN SUPERSONIC CROSSFLOWS USING A PRE-DETONATOR J Vargas, J Sosa, D Rosato, K Ahmed ASTFE Digital Library, 2018 | | 2018 |
