Experimental results are reported for the response to a favourable pressure
gradient of an initially turbulent boundary layer (Re-theta approximate to
1600) developing on a flat plate with its leading edge skewed at 60 degree
s to the approach flow. The pressure gradient orthogonal to the leading edg
e is nominally the same as that which was shown by Escudier et al. [(1998)
Exp Fluids 25: 491-502] to cause extreme thinning of a two-dimensional (2D)
(i.e. unskewed) turbulent boundary layer and the intermittency in the imme
diate vicinity of the surface to fall to zero, i.e. an apparent laminarisat
ion of the boundary layer. In the case of the skewed boundary layer, the re
sponses of the turbulence and mean-flow structures are qualitatively simila
r to those for the 2D situation. However, the streamwise pressure gradient
is much weaker than for the 2D experiment and the extent of the changes it
produces is much reduced. Even so, the changes are considerably greater tha
n would be expected from the magnitude of the streamwise pressure gradient.