When a column of droplets freely falling from an ultrasonic atomizer w
as ignited behind a reflected shock, no ignition occurred at a tempera
ture below 1100 K, even if the pressure was as high as IMPa. Although,
a higher temperature condition ensured ignition, no luminous flame wa
s observable by high-speed photography, and even if a luminous flame l
ump appeared at an extremely high temperature, it disappeared without
spreading over the entire column of droplets in this case. It is known
however that, if a fuel is injected into a diesel cylinder or an elec
tric furnace, ignition occurs even at a temperature as low as 650 K wi
th a luminous flame spreading over the entire spray. These differences
could be caused by the effects of turbulent mixing between fuel dropl
ets and hot air, in fact, turbulence-generating rods were placed on th
e upstream side of the spray column. Experimental results indicates th
at the ignition limit was lowered to 840 K, and the ignition delay per
iod was decreased by increasing the intensity of turbulence. Furthermo
re, the light emission of the flame was intensified, and normal spray
combustion was maintained in the low-temperature atmosphere after the
shock tube ceased its operation.