Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft
Targeting the nonlinear issues of the canard dual-spin aircraft, which relies on the high-speed rotation of the afterbody for flight stability and achieves trajectory correction by adjusting the roll angle of the low-speed rotating forebody to alter aerodynamics, the establishment of an accurate aer...
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| Autors principals: | , , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2025-06-01
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| Col·lecció: | Aerospace |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2226-4310/12/6/558 |
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