Abstract
An original technology of stability analysis of an airfoil boundary layer is presented in this paper. The technology includes an extraction of the boundary layer from the results of laminar flow computations, the computation of neutral curves and increments of Tollmien-Schlichting waves, and the computation of the location of laminar-turbulent transition zone by the eN-method for a given set of freestream turbulence levels. To be specific,we consider the flow around the NACA23012 airfoil with zero angle of attack at moderate Reynolds numbers.
Keywords: Airfoil; boundary layer; hydrodynamic stability; Tollmien-Schlichting waves; laminar-turbulent transition; eN-method.
Published Online: 2014-7-23
Published in Print: 2014-8-1
© 2014 by Walter de Gruyter Berlin/Boston
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Articles in the same Issue
- Masthead
- Numerical prediction of laminar-turbulent transition on an airfoil
- Orthogonal transformations of differential-difference schemes. Introduction to discrete analysis
- Mixed FE method with piece-wise constant fluxes on polyhedral meshes
- The error analysis for spectral models of the sea surface undulation
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Keywords for this article
Airfoil;
boundary layer;
hydrodynamic stability;
Tollmien-Schlichting waves;
laminar-turbulent transition;
eN-method.
Articles in the same Issue
- Masthead
- Numerical prediction of laminar-turbulent transition on an airfoil
- Orthogonal transformations of differential-difference schemes. Introduction to discrete analysis
- Mixed FE method with piece-wise constant fluxes on polyhedral meshes
- The error analysis for spectral models of the sea surface undulation
- Numerical statistical modelling algorithms for electron avalanches in gases