The breakup of a round water jet by a swirling coaxial annular air jet
, issuing from convergent jet nozzles has been studied experimentally.
The intensity of the swirl and the water to air mass flux ratio have
been varied over a large range. It was found that the liquid jet is li
ttle affected by the swirl when the swirl number, here defined by the
ratio of tangential to axial air jet nozzle velocities, is below a cri
tical value (S-cr). Just above this value the liquid jet undergoes an
explosive radial expansion and disintegration. A simple model shows th
at the physically relevant parameters are the gas to liquid momentum f
lux ratio M and the ratio of the nozzle's diameters. For small momentu
m flux ratios, S-cr was found to depend on M-(1/2) until an asymptotic
constant value is reached at large M. Surface tension has no effect o
n the breakup when air velocities are large, however, membrane-type br
eakup is dominant at the lower air velocities when the aerodynamic Web
er number is of order 100 or less. (C) 1996 American Institute of Phys
ics.