Assessment of spanwise domain size effect on the transitional flow past an airfoil
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Publication:1646693
DOI10.1016/j.compfluid.2015.10.008zbMath1390.76245OpenAlexW2194596842MaRDI QIDQ1646693
Publication date: 26 June 2018
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: http://hdl.handle.net/10754/581352
General aerodynamics and subsonic flows (76G25) Direct numerical and large eddy simulation of turbulence (76F65) Transition to turbulence (76F06)
Related Items (5)
Low-\(Re\) flow past an isolated cylinder with rounded corners ⋮ Drag reduction on a transonic airfoil ⋮ Wall-pressure fluctuations of laminar separation bubble based on direct numerical simulation and experiments over a hydrofoil at \(\mathrm{Re}=450,000\) ⋮ A complementary numerical and experimental study of the influence of Reynolds number on theoretical models for wingtip vortices ⋮ Wall-modelled large-eddy simulation of turbulent flow past airfoils
Uses Software
Cites Work
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