An experiment system was designed for the study of well-defined turbulent n
onpremixed spray flames. Particular emphasis was placed on minimizing the i
nfluence of the injector design and on maximizing turbulence within the spr
ay flames. A comprehensive description of the structure of such flames was
obtained by applying a variety of complementary diagnostic techniques, incl
uding: broadband chemiluminescence imaging, CH* emission-imaging, phase Dop
pler interferometric techniques, and spontaneous Raman spectroscopy. Two me
thanol spray flames were examined in detail, with Reynolds number ranging f
rom 2.1 x 10(4) to 2.8 x 10(4). Flame appearance and detailed measurements
confirmed the occurrence of group combustion. Near the burner mouth, a dens
e column of drops enveloped by a common flame was observed. Further up, lar
ge corrugated structures were visualized which eventually developed into se
parate "islands." A significant fraction of the spray escaped unburned, whi
ch implies that droplet evaporation is slow in this configuration. Detailed
scanning of the flames provided an extensive database of average and fluct
uating components of gas velocity and temperature, as well as spray and dro
plet size-classified properties. Key conclusions from such measurements inc
lude: the evidence of two-way coupling between the two phases along the cen
terline near the burner mouth; a velocity acceleration in the densest areas
of the spray flames, as a result of momentum addition through vaporization
, followed by deceleration farther downstream as the jet spreading predomin
ates; and the droplet inertial behavior, especially for the large size clas
ses, as confirmed by estimates of some relevant Stokes numbers. The average
flame height was found to correlate with an overall equivalence ratio and
with the initial concentration of droplets at the burner mouth. (C) 2000 by
The Combustion Institute.