A detailed computer-visualized flowfield of a row of jets in a confine
d crossflow is presented. The Reynolds-averaged Navier-Stokes equation
s are solved by using a finite volume method that incorporates a parti
al differential equation for incremental pressure to obtain a divergen
ce-free flowfield. The turbulence is described by a multiple-time-scal
e turbulence model. The computational domain includes the upstream reg
ion of the circular jet so that the interaction between the jet and th
e crossflow is simulated accurately. It is shown that the row of jets
in the crossflow is characterized by a highly complex flowfield that i
ncludes a horseshoe vortex and two helical vortices whose secondary ve
locity components are corotating in space. It is also shown that the h
orseshoe vortex is a ring of reversed flows located along the circumfe
rence of the jet exit.