An experimental study is presented for flowfields behind an axially mo
unted cylindrical bluff body of annular swirling jet flows. Both the c
onfined and the unconfined cases are examined. The controlled paramete
rs included the Reynolds number Re and the swirl number S. Smoke strea
ks were used to observe the dynamic flow structures of the recirculati
on zone behind the bluff body. Laser-Doppler anemometry was used for v
elocity measurements at the jet exit and downstream of the annular jet
flows. The results indicate that the recirculation zones for both the
unconfined and the confined cases can be classified into seven typica
l flow patterns based on the Reynolds number and swirl number: stable
how vortex shedding, transition, prepenetration, penetration, vortex b
reakdown, and attachment. The how patterns and their domains in (Re, S
) space for unconfined and confined cases were basically the same. In
the attachment regime, the central recirculation zone for the confined
case was larger than that for the unconfined case. The boundaries of
the recirculation zone for various flow conditions were investigated.
Scaling analysis was used to correlate the lengths of the recirculatio
n zone with the swirl number.