P. Petitjeans et al., EFFECT OF CURVATURE ON THE VELOCITY PROFILE AND BOUNDARY-LAYER IN FLOW-THROUGH A CURVED CHANNEL, La Recherche aerospatiale, (2), 1995, pp. 125-138
We assess the base flow through a curved channel within the framework
of a study of Gortler instability in the boundary layers in how over a
concave wall. The base flow is defined as the flow without the three-
dimensional effects of the instability. We present experimental, analy
tical, and numerical results of flows over curved walls. We address th
e variation of the boundary layer thickness as well as the flow outsid
e the boundary layer. We show that in a curved channel? the two-dimens
ional flow accelerates over the convex wall while it decelerates over
the concave wall. The 2D numerical simulation demonstrates the importa
nce of a longitudinal pressure gradient that always appears in such a
geometry. In addition, we qualitatively discuss some modifications to
the two-dimensional flow under the influence of three-dimensional Ekma
n cells (also called Dean cells) or centrifugal instabilities of the G
ortler or Dean type. We explain the origin of what is commonly known i
n the literature as ''the transition from two to four rolls'' for flow
through a curved channel of square or circular cross section.