1997
DOI: 10.1615/atomizspr.v7.i6.70
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Modeling Atomization Processes of Pressure-Swirl Hollow-Cone Fuel Sprays

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Cited by 179 publications
(92 citation statements)
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“…The injection velocity (U) is dependent on the pressure difference (Δp) between the injection (p inj ) and chamber pressure (p c ): (1) In the original linear instability sheet atomization (LISA) breakup model for pressure-swirl injectors, a velocity coefficient (k v ) is used instead of discharge coefficient (C D ) in Eq. (1), and a correlation for the coefficient has been suggested [36]. Later, Schmidt et al [37] estimated the velocity coefficient from a typical value (0.78) of the discharge coefficient of a single nozzle with sharp inlet corners by reducing the value by 10% for extra momentum losses, such that (2) where θ is the half of spray angle and d n is the nozzle diameter.…”
Section: Numerical Setupmentioning
confidence: 99%
“…The injection velocity (U) is dependent on the pressure difference (Δp) between the injection (p inj ) and chamber pressure (p c ): (1) In the original linear instability sheet atomization (LISA) breakup model for pressure-swirl injectors, a velocity coefficient (k v ) is used instead of discharge coefficient (C D ) in Eq. (1), and a correlation for the coefficient has been suggested [36]. Later, Schmidt et al [37] estimated the velocity coefficient from a typical value (0.78) of the discharge coefficient of a single nozzle with sharp inlet corners by reducing the value by 10% for extra momentum losses, such that (2) where θ is the half of spray angle and d n is the nozzle diameter.…”
Section: Numerical Setupmentioning
confidence: 99%
“…5 2 2 cos ρ σ θ Figure 6. Schematic showing the conceptual liquid flow structure at the nozzle exit and sheet breakup processes [12].…”
Section: Breakup Lengthmentioning
confidence: 99%
“…The atomization process of a liquid fuel jet [14][15][16][17][18], the turbulent dispersion of the resulting droplets [19][20][21][22][23], their interaction with walls [24,25], their evaporation and combustion [26] are phenomena occuring for LES at the subgrid scale and therefore requiring accurate modelling.…”
Section: However Most Les Calculations Consider Only Gaseous Flows Anmentioning
confidence: 99%