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Large eddy simulation of flow separation on an airfoil at a high angle of attack and \(Re = 10^{5}\) using Cartesian grids

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Publication:1020481
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DOI10.1007/s00162-007-0072-zzbMath1161.76519OpenAlexW2018419448MaRDI QIDQ1020481

Rainer Friedrich, Sven Eisenbach

Publication date: 29 May 2009

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00162-007-0072-z



Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Finite volume methods applied to problems in fluid mechanics (76M12)


Related Items (2)

Assessment of spanwise domain size effect on the transitional flow past an airfoil ⋮ On the large-eddy simulations for the flow around aerodynamic profiles using unstructured grids


Uses Software

  • XFOIL


Cites Work

  • LESFOIL: Large eddy simulation of flow around a high lift airfoil. Results of the project LESFOIL, supported by the European Union 1998--2001.
  • A dynamic subgrid-scale eddy viscosity model
  • A Lagrangian dynamic subgrid-scale model of turbulence
  • Iterative Solution of Implicit Approximations of Multidimensional Partial Differential Equations


This page was built for publication: Large eddy simulation of flow separation on an airfoil at a high angle of attack and \(Re = 10^{5}\) using Cartesian grids

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