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Thickness effect of NACA foils on hydrodynamic global parameters, boundary layer states and stall establishment

Article dans une revue avec comité de lecture
Author
ccSARRAF, Christophe
1019 Laboratoire d'énergétique et de mécanique des fluides interne [LEMFI]
DJERIDI, Henda
913 Laboratoire de physique des océans [LPO]
PROTHIN, Sébastien
13094 Institut de Recherche de l'Ecole Navale [IRENAV]
BILLARD, Jean-Yves
13094 Institut de Recherche de l'Ecole Navale [IRENAV]

URI
http://hdl.handle.net/10985/10295
DOI
10.1016/j.jfluidstructs.2010.02.004
Date
2010
Journal
Journal of Fluids and Structures

Abstract

The present study investigates experimentally the hydrodynamic behavior of 2D NACA (15, 25, 35%) symmetric hydrofoils at Reynolds number 0.5 106 . A particular attention is paid on the hysteretic behavior at static stall angle and a detailed cartography of boundary layer structures (integral quantities and velocity profiles) is given in order to put in evidence the mechanism of the detachment and the onset of von Karman instability for thick profile

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