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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...

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Detalles Bibliográficos
Autores principales: Vinuesa, Ricardo, Hosseini, Seyed M., Hanifi, Ardeshir, Henningson, Dan S., Schlatter, Philipp
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Springer Netherlands 2017
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