The effect of twist morphing on aerodynamic performance of finite wing at low Reynolds number
This study experimentally investigates the effect of twist morphing on the aerodynamic characteristics of a finite wing at low Reynolds numbers (Re). As the base model, a NACA 0018 airfoil with an aspect ratio of 4 is used. The twist morphing configuration is obtained by applying camber deflection a...
-д хадгалсан:
| Үндсэн зохиолчид: | , , , , |
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| Формат: | Artigo |
| Хэл сонгох: | Inglês |
| Хэвлэсэн: |
EDP Sciences
2026-01-01
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| Цуврал: | EPJ Web of Conferences |
| Онлайн хандалт: | https://www.epj-conferences.org/articles/epjconf/pdf/2026/14/epjconf_efm2026_01005.pdf |
| Шошгууд: |
Шошго байхгүй, Энэхүү баримтыг шошголох эхний хүн болох!
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