An Experimental Study on Flow Control at Low Reynolds Numbers Using DBD Plasma Actuators on NACA 4412 Airfoil
Flow separation is a crucial issue in aeronautics and astronautics, particularly at low Reynolds numbers. Active flow control (AFC) techniques show promise in addressing this problem. However, further research is needed to fully integrate these systems onto air vehicles. Due to their low weight, and...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Turkish Air Force Academy
2025-01-01
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| coleção: | Havacılık ve Uzay Teknolojileri Dergisi |
| Assuntos: | |
| Acesso em linha: | https://jast.hho.msu.edu.tr/index.php/JAST/article/view/606 |
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