http://www.cnr.it/ontology/cnr/individuo/prodotto/ID276025
Modelling of primary breakup process of a gasoline direct engine multi-hole spray (Articolo in rivista)
- Type
- Label
- Modelling of primary breakup process of a gasoline direct engine multi-hole spray (Articolo in rivista) (literal)
- Anno
- 2013-01-01T00:00:00+01:00 (literal)
- Alternative label
MALAGUTI S., FONTANESI S., CANTORE G., MONTANARO A., ALLOCCA L. (2013)
Modelling of primary breakup process of a gasoline direct engine multi-hole spray
in Atomization and sprays
(literal)
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- MALAGUTI S., FONTANESI S., CANTORE G., MONTANARO A., ALLOCCA L. (literal)
- Pagina inizio
- Pagina fine
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- MALAGUTI S.-DIPARTIMENTO INGEGNERIA-UNIVERSITA' DEGLI STUDI DI MODENA E REGGIO EMILIA
FONTANESI S.-DIPARTIMENTO INGEGNERIA-UNIVERSITA' DEGLI STUDI DI MODENA E REGGIO EMILIA
CANTORE G.-DIPARTIMENTO INGEGNERIA-UNIVERSITA' DEGLI STUDI DI MODENA E REGGIO EMILIA (literal)
- Titolo
- Modelling of primary breakup process of a gasoline direct engine multi-hole spray (literal)
- Abstract
- This paper proposes a numerical methodology for the simulation of a gasoline spray generated by a
multi-hole injector of a current production wall-guided gasoline direct injection engine. Particular
care is dedicated to the accurate representation of the spray primary breakup by means of an atomization
model. The model is purposely implemented to take into account cavitation phenomena and
turbulent effects induced by the nozzle geometry through a simplified approach. Because a high primary
breakup rate is expected, an initial distribution of atomized droplets is predicted at the nozzle
hole exit by the numerical approach. The spray is at first experimentally investigated in a test vessel
at non-evaporative ambient conditions and under quiescent conditions, in which commercial gasoline
is injected at two different injection pressures (10.0 and 20.0 MPa). The spray is characterized
in terms of both the instantaneous mass flow rate and morphology. Numerical simulations are performed
and then compared against the experiments in order to evaluate their capability to correctly
predict liquid spray penetration, droplet-size distribution, and spray morphology. The new approach
is a fairly simple, yet reliable, solution that is able to predict the influence of the nozzle hole (in terms
of the discharge coefficient, diameter, and length), neglecting geometrical details that are usually far
from being easily accessed by engine developers (literal)
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