An experimental study of the structure of an acoustically forced, reacting
two-phase jet was performed. The jet was acoustically forced to control the
formation and evolution of large-scale structures in the near field of the
jet. Phase-locked data acquisition techniques were used to correlate dropl
et statistics and dynamics with features of the large-scale structures. Pha
se Doppler interferometry was used to acquire droplet statistics. Planar im
aging techniques were applied to document the distribution of droplets with
in the jet. The results show that the interaction between droplets and larg
e-scale structures leads to a nonuniform distribution of droplets in the re
acting jet. The combination of transport effects and droplet evaporation le
ads to the formation of droplet clusters. The group combustion behavior of
the droplet field was evaluated by estimating the group combustion number f
rom experimental data. External sheath burning is present in the early port
ion of the flame followed by a transition to external group combustion as c
lusters begin to be the dominant feature. Late in the cluster lifetime ther
e is a shift to internal group combustion. (C) 2000 by The Combustion Insti
tute.