Aero-propulsive coupling modeling and dynamic stability analysis of distributed electric propulsion tandem-wing UAV with rapid ascent capability-Reference-Cited by-同舟云学术

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Aero-propulsive coupling modeling and dynamic stability analysis of distributed electric propulsion tandem-wing UAV with rapid ascent capability

Published:2024-10 Issue: Volume:153 Page:109406
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Qin Jiachen,Zhou Zhou,Yang Guowei,Shao Zhuang,Zong Jia

Publisher

Elsevier BV

Reference28 articles.

1. Numerical simulation of distributed propulsion systems using CFD;Qiao;Aerosp. Sci. Technol.,2024

2. Home | Electra. Aero Available online: https://www.electra.aero/(accessed on 9 January 2024).

3. Flight test results of a subscale super-STOL aircraft, Proceedings of the AIAA Scitech 2020 Forum;Courtin,2020

4. Computational analysis of a wing designed for the X-57 distributed electric propulsion aircraft;Deere,2017

5. Dynamic modeling and analysis of tilt-wing electric vertical take-off and landing vehicles;May,2022

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