Study on longitudinal stability of ducted vertical take-off and landing fixed-wing UAV
The longitudinal flight stability of the ducted vertical take-off and landing fixed-wing UAV during the flight state of hovering and transition is studied. Firstly, based on the Blade-Element Momentum Theory (BEMT) and experimental data, a coaxial dual-rotor ducted aerodynamic model and a thrust duc...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2021-08-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/04/jnwpu2021394p712/jnwpu2021394p712.html |