Article ID Journal Published Year Pages File Type
6638531 Fuel 2014 13 Pages PDF
Abstract
A numerical methodology, based on a preliminary Eulerian Steady Simulation of the nozzle, has been developed in order to gain correct flow rates and turbulence data at each of the nozzle holes exit. Then the Lagrangian spray simulations have been carried out by means of a new atomization approach able to take into account the cavitation phenomena and the turbulence effects. A tuning campaign has been performed in order to validate the secondary KH-RT breakup model, and a grid sensitivity analysis has been carried out.
Keywords
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Physical Sciences and Engineering Chemical Engineering Chemical Engineering (General)
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