Theoretical spray performance of swirl-type nozzles was developed by s
olving boundary flows in the swirl chamber of the nozzle using the int
egral momentum method. Essential structures of the discharge coefficie
nt, the swath coefficient, and the volume median diameter were derived
from the theoretical investigation of fluid motion. The nozzle parame
ters and average relative velocity at the discharge orifice governed t
he spray performance and flow regions. Extreme conditions that sensiti
vely influenced the spray performance at high and low flow rates were
identified from the theoretical analysis. The theoretical spray perfor
mance discussed in this study would be a basic form for the design of
a variable flow swirl nozzle, and be subject to calibration for a spec
ific configuration of the swirl nozzle.