Morphing wing airfoil optimization for small unmanned aviation vehicle
Modern small unmanned aerial vehicles (UAVs) perform a wide range of missions, requiring high efficiency in various, often conflicting, flight conditions. Conventional airfoils, optimized for a single specific condition, exhibit suboptimal performance in others, limiting the overall flight capabilit...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Russo |
| Publicat: |
Moscow State Technical University of Civil Aviation
2026-07-01
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| Col·lecció: | Научный вестник МГТУ ГА |
| Matèries: | |
| Accés en línia: | https://avia.mstuca.ru/jour/article/view/2780 |
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