Á lódáil...
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...
Na minha lista:
| Príomhúdar: | |
|---|---|
| Formáid: | Artigo |
| Teanga: | Inglês |
| Foilsithe: |
Isfahan University of Technology
2022-03-01
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| Sraith: | Journal of Applied Fluid Mechanics |
| Ábhair: | |
| Rochtain Ar Líne: | https://www.jafmonline.net/article_2024_a48e875a20b48ff98195645bb8a059c8.pdf |
| Clibeanna: |
Cuir Clib Leis
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