Simulation of the complex flow inside a sharp U-bend needs both refined tur
bulence models and higher order numerical discretization schemes. In the pr
esent study, a non-linear low-Reynolds number (low-Re) k-omega model includ
ing the cubic terms was employed to predict the turbulent flow through a sq
uare cross-sectioned U-bend with a sharp curvature, R-C/D = 0.65. In the tu
rbulence model employed for the present study, the cubic terms are incorpor
ated to represent the effect of extra strain-rates such as streamline curva
ture and three-dimensionality on both turbulence normal and shear stresses.
In order to accurately predict such complex flowfields, a higher-order bou
nded interpolation scheme (Song et al., 1999) has been used to discretize a
ll the transport equations. The calculated results by using both the non-li
near k-omega model and the linear low-Reynolds number k-epsilon model (Laun
der and Sharma, 1974) have been compared with experimental data. It is show
n that the present model produces satisfactory predictions of the flow deve
lopment inside the sharp U-bend and well captures the characteristics of th
e turbulence anisotropy within the duct core region and wall sub-layer.