| A zonal Galerkin-free POD model for incompressible flows M Bergmann, A Ferrero, A Iollo, E Lombardi, A Scardigli, H Telib Journal of Computational Physics 352, 301-325, 2018 | 51 | 2018 |
| Field inversion for data-augmented RANS modelling in turbomachinery flows A Ferrero, A Iollo, F Larocca Computers & Fluids 201, 104474, 2020 | 32 | 2020 |
| A robust and adaptive recovery‐based discontinuous Galerkin method for the numerical solution of convection–diffusion equations A Ferrero, F Larocca, G Puppo International Journal for Numerical Methods in Fluids 77 (2), 63-91, 2015 | 28 | 2015 |
| Registration-based model reduction of parameterized two-dimensional conservation laws A Ferrero, T Taddei, L Zhang Journal of Computational Physics 457, 111068, 2022 | 23 | 2022 |
| Turbomachinery design by a swarm-based optimization method coupled with a CFD solver E Ampellio, F Bertini, A Ferrero, F Larocca, L Vassio Advances in aircraft and spacecraft science 3 (2), 149, 2016 | 19 | 2016 |
| Control of a supersonic inlet in off-design conditions with plasma actuators and bleed A Ferrero Aerospace 7 (3), 32, 2020 | 18 | 2020 |
| Global and local POD models for the prediction of compressible flows with DG methods A Ferrero, A Iollo, F Larocca International Journal for Numerical Methods in Engineering 116 (5), 332-357, 2018 | 18 | 2018 |
| Feedback filtering in discontinuous Galerkin methods for Euler equations A Ferrero, F Larocca Progress in Computational Fluid Dynamics, an International Journal 16 (1), 14-25, 2016 | 17 | 2016 |
| Differential throttling and fluidic thrust vectoring in a linear aerospike M Ferlauto, A Ferrero, M Marsicovetere, R Marsilio International Journal of Turbomachinery, Propulsion and Power 6 (2), 8, 2021 | 16 | 2021 |
| Unstructured discretisation of a non-local transition model for turbomachinery flows A Ferrero, F Larocca, V Bernaschek Advances in aircraft and spacecraft science 4 (5), 555, 2017 | 14 | 2017 |
| Adaptive cfd schemes for aerospace propulsion A Ferrero, F Larocca Journal of Physics: Conference Series 841 (1), 012017, 2017 | 13 | 2017 |
| Plasma actuator–assisted rocket nozzle for improved launcher performance A Ferrero, D Pastrone AIAA Journal 57 (4), 1348-1354, 2019 | 10 | 2019 |
| Fluidic control of transition in a dual-bell nozzle A Ferrero, E Martelli, F Nasuti, D Pastrone AIAA Propulsion and Energy 2020 Forum, 3788, 2020 | 8 | 2020 |
| Dual-bell nozzle for space launchers with fluidic control of transition A Ferrero, A Conte, E Martelli, F Nasuti, D Pastrone AIAA Propulsion and Energy 2021 Forum, 3586, 2021 | 7 | 2021 |
| Fluidic thrust vectoring for annular aerospike nozzle M Ferlauto, A Ferrero, R Marsilio AIAA Propulsion and Energy 2020 Forum, 3777, 2020 | 6 | 2020 |
| RANS closure approximation by artificialneural networks A Ferrero, A Iollo, F Larocca ETC 2019-13th European Turbomachinery Conference on Turbomachinery Fluid …, 2019 | 6 | 2019 |
| Shock vector control technique for aerospike nozzles M Ferlauto, A Ferrero, R Marsilio AIAA Scitech 2020 Forum, 2246, 2020 | 5 | 2020 |
| CFD-based Fluidic Thrust Vectoring model for fighter aircraft E Capello, A Ferrero, R Marsilio, M Ferlauto AIAA Propulsion and Energy 2019 Forum, 4311, 2019 | 5 | 2019 |
| Numerical tool optimization for advanced rocket nozzle performance prediction A Conte, A Ferrero, F Larocca, D Pastrone AIAA Propulsion and Energy 2019 Forum, 4115, 2019 | 5 | 2019 |
| Dual-bell nozzle with fluidic control of transition for space launchers A Ferrero, A Conte, E Martelli, F Nasuti, D Pastrone Acta Astronautica 193, 130-137, 2022 | 4 | 2022 |
Angelo IolloInstitut de Mathématiques de Bordeaux, Université de Bordeaux and InriaBestätigte E-Mail-Adresse bei math.u-bordeaux.fr
