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Critical Angle and Fundamental Frequency of Symmetric Airfoils at Low Reynolds Numbers
The unsteady vortex evolution of NACA 0012 airfoil is numerically investigated at low angles of attack ranging from 0° to 10° where the separation is performed from the trailing edge. The Reynolds number ranges between 1000 and 4000. The laminar separation bubble at the trailing edge is observed and...
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| Hoofdauteur: | |
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| Formaat: | Artigo |
| Taal: | Inglês |
| Gepubliceerd in: |
Isfahan University of Technology
2022-03-01
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| Reeks: | Journal of Applied Fluid Mechanics |
| Onderwerpen: | |
| Online toegang: | https://www.jafmonline.net/article_2024_a48e875a20b48ff98195645bb8a059c8.pdf |
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