Open Access
Issue |
JNWPU
Volume 39, Number 1, February 2021
|
|
---|---|---|
Page(s) | 27 - 36 | |
DOI | https://doi.org/10.1051/jnwpu/20213910027 | |
Published online | 09 April 2021 |
- Kong Xianghao, Zhang Zhuoran, Lu Jiawei, et al. Review of electric power system of distributed electric propulsion aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 46–62 (in Chinese) [Google Scholar]
- Huang Jun, Yang Fengtian. Development and challenges of electric aircraft with new energies[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 62–73 [Article] (in Chinese) [Google Scholar]
- Gohardani A S, Doulgeris G, Singh R. Challenges of future aircraft propulsion: a review of distributed propulsion technology and its potential application for the all electric commercial aircraft[J]. Progress in Aerospace Sciences, 2011, 47(5): 369–391 [Article] [Google Scholar]
- Kim H D, Perry A T, Ansell P J. A review of distributed electric propulsion concepts for air vehicle technology[C]//2018 AIAA/IEEE Electric Aircraft Technologies Symposium, 2018: 4998 [Google Scholar]
- Pieper K, Perry A, Ansell P, et al. Design and development of a dynamically, scaled distributed electric propulsion aircraft testbed[C]//2018 AIAA/IEEE Electric Aircraft Technologies Symposium, 2018: 4996 [Google Scholar]
- De Vries R, Brown M, Vos R. Preliminary sizing method for hybrid-electric distributed-propulsion aircraft[J]. Journal of Aircraft, 2019, 56(6): 2172–2188 [Article] [Google Scholar]
- Hoogreef M, Vos R, De Vries R, et al. Conceptual assessment of hybrid electric aircraft with distributed propulsion and boosted turbofans[C]//AIAA Scitech 2019 Forum, 2019: 1807 [Google Scholar]
- Finger D F, Braun C, Bil C. An initial sizing methodology for hybrid-electric light air-craft[C]//2018 Aviation Technology, Integration, and Operations Conference, 2018: 4229 [Google Scholar]
- Wang S, Economou J T, Tsourdos A. Design of a distributed hybrid electric propulsion system for a light aircraft based on genetic algorithm[C]//AIAA Propulsion and Energy 2019 Forum, 2019: 4305 [Google Scholar]
- Wang S, Economou J T, Tsourdos A. Indirect engine sizing via distributed hybrid-electric unmanned aerial vehicle state-of-charge-based parametrisation criteria[J]. Journal of Aerospace Engineering, 2019, 233(14): 5360–5368 [Article] [Google Scholar]
- Finger D F. Comparative performance and benefit assessment of VTOL and CTOL UAVs[C]//65 Deutsche Gesellschaft Für Luft-und Raumfahrt-Lilienthal-Oberth, Brunswick, Germany, 2016 [Google Scholar]
- Finger D F, Braun C, Bil C. Impact of electric propulsion technology and mission requirements on the performance of VTOL UAVs[J]. CEAS Aeronautical Journal, 2019, 10(3): 827–843 [Article] [Google Scholar]
- Jong T, Slingerland R. Analysis of the twin-fuselage configuration and its h-cabin derivative[C]//AIAA's 3rd Annual Aviation Technology, Integration, and Operations Forum, 2003: 6811 [Google Scholar]
- Perry A T, Ansell P J, Kerho M. Aero-propulsive and propulsor cross-coupling effects on a distributed propulsion system[C]//2018 AIAA Aerospace Sciences Meeting, 2018: 2051 [Google Scholar]
- Tao Fuxing, Zhang Heng, Li Jie. The aerodynamic design of small man-portable loitering munition[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015, 35(6): 111–114 [Article] (in Chinese) [Google Scholar]
- Zamboni J, Vos R, Emeneth M, et al. A method for the conceptual design of hybrid electric aircraft[C]//AIAA Scitech 2019 Forum, 2019: 1587 [Google Scholar]
- Patterson M D, German B J, Moore M D. Performance analysis and design of on-demand electric aircraft concepts[C]//12th AIAA Aviation Technology, Integration and Operations Conference, 2012: 5474 [Google Scholar]
- Aktas Y O, Ozdemir U, Dereli Y, et al. Rapid prototyping of a fixed-wing VTOL UAV for design testing[J]. Journal of Intelligent & Robotic Systems, 2016, 84(1/2/3/4): 639–664 [Article] [Google Scholar]
- Barufald G, Morales M, Silva R G. Energy optimal climb performance of electric aircraft[C]//AIAA Scitech 2019 Forum, 2019: 0830 [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.