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The effects of injector nozzle geometry and operating pressure conditions on the transient fuel spray behavior
Authors:Email author" target="_blank">Ja?Ye?KooEmail author
Affiliation:(1) School of Aerospace and Mechanical Engineering, Hankuk Aviation University, 412-791 Kyunggi-do, Korea
Abstract:Effects of injector nozzle geometry and operating pressure conditions such as opening pressure, ambient pressure, and injection pressure on the transient fuel spray behavior have been examined by experiments. In order to clarify the effect of internal flow inside nozzle on the external spray, flow details inside model nozzle and real nozzle were also investigated both experimentally and numerically. For the effect of injection pressures, droplet sizes and velocities were obtained at maximum line pressure of 21 MPa and 105 MPa. Droplet sizes produced from the round inlet nozzle were larger than those from the sharp inlet nozzle and the spray angle of the round inlet nozzle was narrower than that from the sharp inlet nozzle. With the increase of opening pressure, spray tip penetration and spray angle were increased at both lower ambient pressure and higher ambient pressure. The velocity and size profiles maintained similarity despite of the substantial change in injection pressure, however, the increased injection pressure produced a higher percentage of droplet that are likely to breakup.
Keywords:Nozzle Geometry  Operating Pressure  Spray Development  Droplet
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