The transitional process of a forced plane wall jet is studied both experim
entally and numerically. Experimentally, particle Image Velocimetry (PIV) a
nd laser-sheet/smoke flow-visualization techniques are implemented to provi
de an overall understanding of the flow features. Numerically, time-accurat
e computational results are obtained by solving the two-dimensional, unstea
dy Navier-Stokes equations. Comparison of PIV data and two-dimensional comp
uted results shows excellent agreement in the early stages of transition, d
emonstrating that the numerical study can be used to complement the experim
ental one. The results show that; under the influence of external excitatio
n, linear-instability growth is bypassed and a discrete shear-layer vortex
is formed in the immediate vicinity of the nozzle exit. This vortex interac
ts with the boundary-layer vorticity, leading to the formation of another v
ortex in the inner layer. These two vortices form a vortex couple that for
high forcing convects downstream in a stable manner. By adoption of either
a no-slip or a slip boundary condition in the numerical computation, it is
determined that the flow development is relatively insensitive to the impos
ed wall-boundary condition. This seems to suggest that the physical mechani
sm leading to the formation of the boundary-layer vortex is an inviscid rot
ational one.