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Measuring air core characteristics of a pressure-swirl atomizer via a transparent acrylic nozzle at various Reynolds numbers

Authors
Lee, E.J.Oh, S.Y.Kim, H.Y.James, S.C.Yoon, S.S.
Issue Date
2010
Keywords
Air core; Fuel injector performance; Swirl spray; Temperature effect
Citation
Experimental Thermal and Fluid Science, v.34, no.8, pp.1475 - 1483
Indexed
SCIE
SCOPUS
Journal Title
Experimental Thermal and Fluid Science
Volume
34
Number
8
Start Page
1475
End Page
1483
URI
https://scholar.korea.ac.kr/handle/2021.sw.korea/118327
DOI
10.1016/j.expthermflusci.2010.07.010
ISSN
0894-1777
Abstract
Because of thermal fluid-property dependence, atomization stability (or flow regime) can change even at fixed operating conditions when subject to temperature change. Particularly at low temperatures, fuel's high viscosity can prevent a pressure-swirl (or simplex) atomizer from sustaining a centrifugal-driven air core within the fuel injector. During disruption of the air core inside an injector, spray characteristics outside the nozzle reflect a highly unstable, nonlinear mode where air core length, Sauter mean diameter (SMD), cone angle, and discharge coefficient variability. To better understand injector performance, these characteristics of the pressure-swirl atomizer were experimentally investigated and data were correlated to Reynolds numbers (Re). Using a transparent acrylic nozzle, the air core length, SMD, cone angle, and discharge coefficient are observed as a function of Re. The critical Reynolds numbers that distinguish the transition from unstable mode to transitional mode and eventually to a stable mode are reported. The working fluids are diesel and a kerosene-based fuel, referred to as bunker-A. © 2010 Elsevier Inc.
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