Numerical study of airfoil stall cells using a very wide computational domain

DOI10.1016/j.compfluid.2016.09.023zbMath1390.76681OpenAlexW2529451642MaRDI QIDQ1647172

Pierre-Luc Delafin, Luca Manni, Takafumi Nishino

Publication date: 26 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: http://dspace.lib.cranfield.ac.uk/handle/1826/10810

zbMATH Keywords

flow separationunsteady RANS2D/3D transitiondelayed DEShigh aspect ratio wing

Mathematics Subject Classification ID

Related Items (3)

Numerical analysis on the oscillation of stall cells over a NACA 0012 aerofoil ⋮ Link between subsonic stall and transonic buffet on swept and unswept wings: from global stability analysis to nonlinear dynamics ⋮ Bifurcation scenario for a two-dimensional static airfoil exhibiting trailing edge stall

Cites Work

• Unnamed Item
• On the birth of stall cells on airfoils
• Development of DDES and IDDES formulations for the \(k\)-\(\omega \) shear stress transport model
• A new version of detached-eddy simulation, resistant to ambiguous grid densities

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