Effects of Fixed Leading-Edge DBD Plasma Actuation on Pressure-Derived Lift of a NACA 0012 Airfoil
In this study, a dielectric barrier discharge (DBD) plasma actuator was placed at the leading edge of a National Advisory Committee for Aeronautics (NACA) 0012 airfoil to act on the separation initiation point, rather than on an already separated flow farther downstream on the upper surface. The aer...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2026-02-01
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| Col·lecció: | Aerospace |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2226-4310/13/2/163 |
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