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Decelerating boundary layer : a new scaling and mixing length model

type de publication      article dans une revue internationale avec comité de lecture
date de publication 2003
auteur(s) Bernard Anthony; Foucaut Jean-Marc; Dupont Patrick; Stanislas Michel
journal (abréviation) American Institute of Aeronautics and Astronautics (AIAA)
volume (numéro) 41 (2)
  
pages 248 – 255
résumé A model experiment has been designed in the frame of a coordinated European project called AEROMEMS. This model is a 2D bump in a boundary layer wind tunnel, which mimics the adverse pressure gradient on the suction side of an airfoil at the verge of separation. The flow is characterized mainly by hot wire anemometry. The integral parameters and the mean velocity profiles are compared to existing models and to Navier Stokes computations. A new scaling and a new mixing length model are proposed and validated also on the Ludwig & Tillman data.
mots clés Turbulent boundary layer, Adverse pressure gradient
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