Experimental Study of Flow Around Stepped NACA 0015 Airfoils at Low Reynolds Numbers
This study investigates the flow around Kline-Fogleman (KF) airfoils using Particle Image Velocimetry (PIV) in a wind tunnel at Reynolds number Re = 6.8 × 10<sup>4</sup>. Three configurations are tested: a clean NACA 0015 airfoil and two modified versions with a step on either the pressure or suctio...
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| Asıl Yazarlar: | , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
MDPI AG
2026-01-01
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| Seri Bilgileri: | Engineering Proceedings |
| Konular: | |
| Online Erişim: | https://www.mdpi.com/2673-4591/121/1/18 |
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