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Pressure-Gradient Turbulent Boundary Layers Developing Around a Wing Section
A direct numerical simulation database of the flow around a NACA4412 wing section at R e (c) = 400,000 and 5(∘) angle of attack (Hosseini et al. Int. J. Heat Fluid Flow 61, 117–128, 2016), obtained with the spectral-element code Nek5000, is analyzed. The Clauser pressure-gradient parameter β ranges...
| Autores principales: | , , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Springer Netherlands
2017
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6044240/ https://www.ncbi.nlm.nih.gov/pubmed/30069159 http://dx.doi.org/10.1007/s10494-017-9840-z |