Combined aerodynamic and electrostatic atomization of dielectric liquid jets
Combined aerodynamic and electrostatic atomization of dielectric liquid jets
The electrical and atomization performance of a plane-plane charge injection atomizer using a dielectric liquid, and operating at pump pressures ranging from 15 to 35 bar corresponding to injection velocities of up to 50m/s, is explored via low current electrical measurements, spray imaging and phase Doppler anemometry (PDA). The work is aimed at understanding the contribution of electrostatic charging relevant to typical higher pressure fuel injection systems such as those employed in the aeronautical, automotive and marine sectors. Results show that mean specific charge increases with injection velocity significantly. The effect of electrostatic charge is advantageous at the 15-35 bar range and an arithmetic mean diameter D10 as low as 0.2d is achievable in the spray core and lower still in the periphery where d is the orifice diameter. Using the data available from this higher pressure system and from previous high Reynolds number systems [1], the promotion of primary atomization has been analyzed by examining the effect that charge has on liquid jet surface and liquid jet bulk instability. The results suggest that for the low charge density Qv~2C/m3 cases under consideration here, a significant increase in primary atomization is observed due to a combination of electrical and aerodynamic forces acting on the jet surface, attributed to the significantly higher jet Weber number (Wej) when compared to low injection pressure cases. Analysis of Sauter mean diameter (SMD) results show that for jets with elevated specific charge density of the order QV~6C/m3, the jet creates droplets that a conventional turbulent jet would, but with a significantly lower power requirement. This suggests that “turbulent” primary atomization, the turbulence being induced by electrical forces, may be achieved under injection pressures that would produce laminar jets.
221-235
Kourmatzis, Agissilaos
2e6a16aa-3a9e-42ae-8e1d-a9b7bf9d637d
Ergene, Egemen L.
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Shrimpton, John S.
9cf82d2e-2f00-4ddf-bd19-9aff443784af
Kyritsis, Dimitros C.
deac92bb-0870-4ffc-a913-b0709e4cd5a1
Mashayek, Farzad
17d01292-40ce-4e5f-8156-d24252268fac
Huo, Ming
dfbe262d-5dbc-4312-9fb9-9e8994320231
July 2012
Kourmatzis, Agissilaos
2e6a16aa-3a9e-42ae-8e1d-a9b7bf9d637d
Ergene, Egemen L.
b6d5e1d4-44a5-4437-a812-0fe97544846b
Shrimpton, John S.
9cf82d2e-2f00-4ddf-bd19-9aff443784af
Kyritsis, Dimitros C.
deac92bb-0870-4ffc-a913-b0709e4cd5a1
Mashayek, Farzad
17d01292-40ce-4e5f-8156-d24252268fac
Huo, Ming
dfbe262d-5dbc-4312-9fb9-9e8994320231
Kourmatzis, Agissilaos, Ergene, Egemen L., Shrimpton, John S., Kyritsis, Dimitros C., Mashayek, Farzad and Huo, Ming
(2012)
Combined aerodynamic and electrostatic atomization of dielectric liquid jets.
Experiments in Fluids, 53 (1), .
(doi:10.1007/s00348-012-1284-6).
Abstract
The electrical and atomization performance of a plane-plane charge injection atomizer using a dielectric liquid, and operating at pump pressures ranging from 15 to 35 bar corresponding to injection velocities of up to 50m/s, is explored via low current electrical measurements, spray imaging and phase Doppler anemometry (PDA). The work is aimed at understanding the contribution of electrostatic charging relevant to typical higher pressure fuel injection systems such as those employed in the aeronautical, automotive and marine sectors. Results show that mean specific charge increases with injection velocity significantly. The effect of electrostatic charge is advantageous at the 15-35 bar range and an arithmetic mean diameter D10 as low as 0.2d is achievable in the spray core and lower still in the periphery where d is the orifice diameter. Using the data available from this higher pressure system and from previous high Reynolds number systems [1], the promotion of primary atomization has been analyzed by examining the effect that charge has on liquid jet surface and liquid jet bulk instability. The results suggest that for the low charge density Qv~2C/m3 cases under consideration here, a significant increase in primary atomization is observed due to a combination of electrical and aerodynamic forces acting on the jet surface, attributed to the significantly higher jet Weber number (Wej) when compared to low injection pressure cases. Analysis of Sauter mean diameter (SMD) results show that for jets with elevated specific charge density of the order QV~6C/m3, the jet creates droplets that a conventional turbulent jet would, but with a significantly lower power requirement. This suggests that “turbulent” primary atomization, the turbulence being induced by electrical forces, may be achieved under injection pressures that would produce laminar jets.
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Published date: July 2012
Organisations:
Engineering Science Unit
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Local EPrints ID: 300716
URI: http://eprints.soton.ac.uk/id/eprint/300716
ISSN: 0723-4864
PURE UUID: f7fc4064-af7f-4eff-b0f2-7e2c80024202
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Date deposited: 29 Feb 2012 14:23
Last modified: 14 Mar 2024 10:25
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Author:
Agissilaos Kourmatzis
Author:
Egemen L. Ergene
Author:
Dimitros C. Kyritsis
Author:
Farzad Mashayek
Author:
Ming Huo
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