Resumen: [EN] Airblast atomization is commonly used to atomize fuel in aircraft engines. An annular liquid sheet is atomized by
the shear forces exerted by the co-flowing air stream. Nevertheless, this technique is less effective in some
specific cases, e.g. when the external air flow velocity is relatively low. Electrohydrodynamic (EHD) atomization
can constitute a solution in these cases. It consists of applying an electric field between two electrodes and
electrically charging the passing carburant. This phenomenon will create instabilities within the liquid, provoking
therefore its atomization. The main objective is therefore to electrically atomize a liquid sheet without the
application of an external air flow like in airblast atomizers.
This paper presents a novel actuator, based on dielectric barrier injection, used to induce instabilities within a
plane liquid sheet of fuel similar to the annular sheet in aircraft engines. The behaviour of this atomizer was
described in previous works. Several modes were observed, sometimes leading to a complete atomization, or just
inducing instabilities and oscillating the liquid sheet. In the present study, only the cases where the liquid sheet is
completely atomized are investigated. Images were recorded with the help of a high speed camera. Primary
atomization is only studied, secondary atomization being neglected. The properties of the spray obtained by EHD
atomization are investigated thoroughly, namely the breakup length, the mesh size, the drople t diameter, the
droplet count, etc.
