The numerical modeling of partially cavitating foils under a confined flow
configuration is described. A complete study of previous numerical models h
ighlights that the presence of a turbulent and two-phase wake, at the rear
of the cavity, has a nonnegligible effect on the local pressure coefficient
, the cavitation number, the cavity length and the lift coefficient; hence
viscous effects must be included. Two potential methods are used, each bein
g coupled with a calculation of the boundary layer developed downstream of
the cavity. So, an open cavity" numerical model, as it is called, was devel
oped and tested with two types of foil: a NACA classic foil and a foil of w
hich the profile is obtained performing an inverse calculation on a propell
er blade test section. On the other hand, under noncavitating conditions, f
or each method, the results are compared with the results obtained by the N
avier-Stokes solver "FLUENT. The cavitating flow configurations presented h
erein were carried out using the small hydrodynamic tunnel at Bassin d'Essa
is des Carenes [Val de Reuil, France]. The results obtained by the two meth
ods are compared with experimental measurements.