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Memorias de investigación
Communications at congresses:
RNS computations of the boundary layer flow over grooved plate
Year:2010
Research Areas
  • Aeronautical engineering
Information
Abstract
We use the Reduced Navier- Stokes equations (RNS) to compute the evolution of the 3d boundary layer flow over a plate with small depth streamwise grooves carved in it. The RNS are derived from the Navier-Stokes equations for flows with large Re number with one slow scale and two short scales. The resulting RNS are nonlinear and fully parabolic equations. In this work we comment the details of the numerical integration of the RNS, where we use a conformal mapping to include the effect of the grooved bottom. We present the resulting flow structures due to the geometry of the problem, also a parametric study to evaluate the effect of the spanwise wave number over the flow configuration. The RNS computations are much more less CPU costly than full 3D DNS, and does not exhibit the numerical instabilities present in previous PSE calculations. Prefer Oral Session X Prefer
International
Si
Congress
63rd Annual Meeting of the American Physical Society
960
Place
Reviewers
Si
ISBN/ISSN
0003-0503
Start Date
21/11/2010
End Date
23/11/2010
From page
254
To page
254
Program of the 63rd Annual Meeting of the Division of Fluid Dynamics
Participants
  • Autor: Carlos Martel Escobar (UPM)
  • Autor: Juan Angel Martin Bautista (UPM)
Research Group, Departaments and Institutes related
  • Creador: Grupo de Investigación: Dinámica y estabilidad no lineal en ingeniería aeroespacial
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