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Numerical studies of spray breakup in a gasoline direct injection (GDI) engine

机译:汽油直喷(GDI)发动机喷雾破裂的数值研究

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The objective of this study is to investigate Spray Breakup process of sprays injected from single and two-hole nozzles for gasoline direct Injection (GDI) engines by using three dimensional CFD code. Spray characteristics were examined for spray tip penetration and other characteristics including: the vapor phase concentration distribution and droplet spatial distribution, which were acquired using the computational fluid dynamics (CFD) simulation. Results showed that as the hole-axis-angle (γ) of the two-hole nozzle decreased, the droplet coalescence increased and vapor mass decreased. The spray with cone angle (θ0) 5 deg for single hole nozzle has the longest spray tip penetration and the spray with the γ of 30 deg and spray cone angle θ0=30 deg for two hole nozzles had the shortest one. Also, when the spray cone angle (θ0) and hole-axis-angle (γ) increased from 5 to 30 deg, the Sauter mean diameter (SMD) decreased for both single-hole and two-hole nozzles used in this study. For a single-hole nozzle, when spray cone angle increased from 5 to 30 deg, the vaporization rate very much because of low level of coalescence. The result of model for tip penetration is good agreement with the corresponding experimental data in the literatures.
机译:这项研究的目的是研究使用三维CFD代码从汽油直喷(GDI)发动机的单孔和两孔喷嘴喷射的喷雾的喷雾破裂过程。检查喷雾特征的喷雾尖端渗透性和其他特征,包括:气相浓度分布和液滴空间分布,这些特征是使用计算流体动力学(CFD)模拟获得的。结果表明,随着两孔喷嘴的孔轴角(γ)的减小,液滴的聚结增加,蒸汽量减小。对于单孔喷嘴,锥角(θ0)为5度的喷雾具有最长的喷嘴尖端穿透,对于两个孔喷嘴,γ为30度且锥角为θ0= 30度的喷雾具有最短的喷雾。同样,当喷雾锥角(θ0)和孔轴角(γ)从5度增加到30度时,本研究中使用的单孔和双孔喷嘴的索特平均直径(SMD)都会减小。对于单孔喷嘴,当喷雾锥角从5度增加到30度时,由于聚结程度低,因此蒸发速度非常高。针尖穿透模型的结果与文献中相应的实验数据吻合良好。

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