Aerodynamic analysis of SD7037 airfoil with flex-skin flap at low angles of attack and low Reynolds numbers
This work concentrates on the effect of a flex-skin trailing edge flap on the aerodynamic characteristics of SD7037 airfoil at low Reynolds numbers, in the range of 2·105 to 5·105 using computational methods. The study used a range of angle of attack (AOA) associated with the take-off phase and diff...
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| Auteurs principaux: | , , |
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| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
ITMO University
2025-12-01
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| Collection: | Научно-технический вестник информационных технологий, механики и оптики |
| Sujets: | |
| Accès en ligne: | https://ntv.elpub.ru/jour/article/view/554 |
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