| Preliminary sizing method for hybrid-electric distributed-propulsion aircraft R De Vries, M Brown, R Vos Journal of Aircraft 56 (6), 2172-2188, 2019 | 151 | 2019 |
| Aerodynamic interaction between propellers of a distributed-propulsion system in forward flight R de Vries, N van Arnhem, T Sinnige, R Vos, LLM Veldhuis Aerospace Science and Technology 118, 107009, 2021 | 89 | 2021 |
| A preliminary sizing method for hybrid-electric aircraft including aero-propulsive interaction effects R de Vries, MT Brown, R Vos 2018 aviation technology, integration, and operations conference, 4228, 2018 | 82 | 2018 |
| Conceptual assessment of hybrid electric aircraft with distributed propulsion and boosted turbofans M Hoogreef, R Vos, R de Vries, LL Veldhuis AIAA Scitech 2019 Forum, 1807, 2019 | 59 | 2019 |
| A comparison of hybrid-electric aircraft sizing methods DF Finger, R de Vries, R Vos, C Braun, C Bil AIAA scitech 2020 forum, 1006, 2020 | 54 | 2020 |
| Range equation for hybrid-electric aircraft with constant power split R De Vries, MFM Hoogreef, R Vos Journal of Aircraft 57 (3), 552-557, 2020 | 51 | 2020 |
| Preliminary sizing of a hybrid-electric passenger aircraft featuring over-the-wing distributed-propulsion R de Vries, M Hoogreef, R Vos AIAA Scitech 2019 Forum, 1811, 2019 | 50 | 2019 |
| Aerodynamic investigation of an over-the-wing propeller for distributed propulsion EA Marcus, R de Vries, A Raju Kulkarni, LL Veldhuis 2018 AIAA Aerospace Sciences Meeting, 2053, 2018 | 49 | 2018 |
| Unsteady pylon loading caused by propeller-slipstream impingement for tip-mounted propellers T Sinnige, R De Vries, BD Corte, F Avallone, D Ragni, G Eitelberg, ... Journal of Aircraft 55 (4), 1605-1618, 2018 | 44 | 2018 |
| Alleviation of propeller-slipstream-induced unsteady pylon loading by a flow-permeable leading edge T Sinnige, BD Corte, R De Vries, F Avallone, R Merino-Martínez, D Ragni, ... Journal of Aircraft 56 (3), 1214-1230, 2019 | 32 | 2019 |
| Engineering method to estimate the blade loading of propellers in nonuniform flow N van Arnhem, R de Vries, T Sinnige, R Vos, G Eitelberg, LLM Veldhuis AIAA Journal 58 (12), 5332-5346, 2020 | 29 | 2020 |
| Synthesis of aero-propulsive interaction studies applied to conceptual hybrid-electric aircraft design M Hoogreef, R de Vries, T Sinnige, R Vos AIAA Scitech 2020 Forum, 0503, 2020 | 24 | 2020 |
| Aero-propulsive efficiency requirements for turboelectric transport aircraft R de Vries, M Hoogreef, R Vos AIAA Scitech 2020 Forum, 0502, 2020 | 24 | 2020 |
| Cross-validation of hybrid-electric aircraft sizing methods DF Finger, R de Vries, R Vos, C Braun, C Bil Journal of Aircraft 59 (3), 742-760, 2022 | 23 | 2022 |
| Aerodynamic performance and interaction effects of circular and square ducted propellers HF Bento, R de Vries, LL Veldhuis AIAA SciTech 2020 Forum, 1029, 2020 | 19 | 2020 |
| Experimental investigation of over-the-wing propeller–boundary-layer interaction R de Vries, N van Arnhem, F Avallone, D Ragni, R Vos, G Eitelberg, ... AIAA Journal 59 (6), 2169-2182, 2021 | 17 | 2021 |
| Aerodynamic Performance Benefits of Over-the-Wing Distributed Propulsion for Hybrid-Electric Transport Aircraft R de Vries, R Vos Journal of Aircraft, 1-18, 2022 | 16 | 2022 |
| Hybrid-Electric Aircraft with Over-the-Wing Distributed Propulsion: Aerodynamic Performance and Conceptual Design R de Vries Delft University of Technology, 2022 | 15 | 2022 |
| Aerodynamic performance and static stability characteristics of aircraft with tail-mounted propellers N van Arnhem, R de Vries, T Sinnige, R Vos, LLM Veldhuis Journal of Aircraft 59 (2), 415-432, 2022 | 12 | 2022 |
| A New Perspective on Battery-Electric Aviation, Part I: Reassessment of Achievable Range RE Wolleswinkel, R de Vries, M Hoogreef, R Vos AIAA SCITECH 2024 Forum, 1489, 2024 | 10 | 2024 |
Roelof VosTU Delft在 tudelft.nl 的电子邮件经过验证
