Aircraft/Engine Integrated Design for an Air-superiority Unmanned Aerial Vehicle

Aiming at the demand of efficient energy management for wide flight envelope of air-superiority unmanned aerial vehicle (UAV), an conceptual and preliminary design of air-superiority UAV with oil-electric hybrid power was proposed based on the idea of integrated aircraft and engine modelling. The ev...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of physics. Conference series 2022-05, Vol.2235 (1), p.12060
Hauptverfasser:	Jianzhi, DENG, Wenyan, SONG, Guangjun, YANG, Feng, JIANG, Neng, XIONG
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Aircraft design Aircraft performance Constraint modelling Design parameters Energy management Flight envelopes Military strategy Performance enhancement Physics Preliminary designs Turbofan engines Unmanned aerial vehicles
Online-Zugang:	Volltext
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