| New insights into the shock tube ignition of H2/O2 at low to moderate temperatures using high-speed end-wall imaging E Ninnemann, B Koroglu, O Pryor, S Barak, L Nash, Z Loparo, J Sosa, ... Combustion and Flame 187, 11-21, 2018 | 88 | 2018 |
| 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), e2102244118, 2021 | 81 | 2021 |
| Experimental evidence of H2/O2 propellants powered rotating detonation waves J Sosa, R Burke, KA Ahmed, DJ Micka, JW Bennewitz, SA Danczyk, ... Combustion and Flame 214, 136-138, 2020 | 44 | 2020 |
| Supersonic driven detonation dynamics for rotating detonation engines J Sosa, KA Ahmed, R Fievisohn, J Hoke, T Ombrello, F Schauer International Journal of Hydrogen Energy 44 (14), 7596-7606, 2019 | 44 | 2019 |
| Compressible turbulent flame speeds of highly turbulent standing flames J Sosa, J Chambers, KA Ahmed, A Poludnenko, VN Gamezo Proceedings of the Combustion Institute 37 (3), 3495-3502, 2019 | 27 | 2019 |
| The evolution of pressure gain in turbulent fast flames HM Chin, J Chambers, J Sosa, A Poludnenko, VN Gamezo, KA Ahmed Combustion and Flame 234, 111641, 2021 | 16 | 2021 |
| Numerical investigation of shock-induced combustion of coal-H2-air mixtures in a unwrapped non-premixed detonation channel M Salvadori, IB Dunn, J Sosa, S Menon, KA Ahmed AIAA Scitech 2020 Forum, 2159, 2020 | 14 | 2020 |
| Flowfield velocity measurements of a rotating detonation engine IB Dunn, J Sosa, M Salvadori, KA Ahmed, S Menon AIAA Scitech 2020 Forum, 1176, 2020 | 13 | 2020 |
| Evaluation of droplet aerodynamic breakup models in supersonic and hypersonic flows A Hess, DA Kessler, RF Johnson, C Aguilera, J Sosa, GB Goodwin AIAA Scitech 2021 Forum, 0751, 2021 | 12 | 2021 |
| Design & development of a hypersonic combustor for oblique detonation wave stabilization J Sosa, K Ahmed 55th AIAA Aerospace Sciences Meeting, 0371, 2017 | 10 | 2017 |
| Numerical investigation of turbulent flame-vortex interaction in premixed cavity stabilized flames CJ Rising, GB Goodwin, RF Johnson, DA Kessler, J Sosa, M Thornton, ... Aerospace Science and Technology 129, 107805, 2022 | 9 | 2022 |
| 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 | 8 | 2021 |
| Exploration of nozzle flow circumferential attenuation and efficient expansion for rotating detonation rocket engines J Sosa, Z Berry, R Burke, KA Ahmed, D Micka AIAA Scitech 2020 Forum, 0197, 2020 | 8 | 2020 |
| Quantification of pressure gain in turbulent fast flames for deflagration-to-detonation HM Chin, J Chambers, J Sosa, KA Ahmed AIAA Scitech 2020 Forum, 0442, 2020 | 8 | 2020 |
| Experimental investigation of detonation wave propagation in a supersonic crossflow J Sosa, K Ahmed, J Hoke, FR Schauer 2018 AIAA aerospace sciences meeting, 0156, 2018 | 8 | 2018 |
| Heat transfer measurements in an elevated pressure RDRE combustor DJ Micka, G Daines, J Sosa, RF Burke, KA Ahmed, E Paulson, ... AIAA Propulsion and Energy 2021 Forum, 3685, 2021 | 7 | 2021 |
| High-Speed Imaging of the Dynamics of H2/O2 Ignition at Low to Moderate Temperatures in a Shock Tube E Ninnemann, O Pryor, S Barak, B Koroglu, J Sosa, K Ahmed, S Vasu 55th AIAA Aerospace Sciences Meeting, 1796, 2017 | 6 | 2017 |
| Experimental validation of rotating detonation for rocket propulsion JW Bennewitz, JR Burr, BR Bigler, RF Burke, A Lemcherfi, T Mundt, ... Scientific Reports 13 (1), 14204, 2023 | 5 | 2023 |
| Velocimetry measurements using structured light-field focusing in a rotating detonation engine J Sosa, K Ahmed, JL Hoke, FR Schauer 2018 AIAA Aerospace Sciences Meeting, 0159, 2018 | 5 | 2018 |
| 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 |
Kareem AhmedProfessor在 ucf.edu 的電子郵件地址已通過驗證
