2009
DOI: 10.4271/2009-01-1355
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Entrainment Waves in Diesel Jets

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Cited by 275 publications
(261 citation statements)
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“…This parameter has been extensively used in many spray studies to characterize the inert spray radial spreading rate [8,25,32,35], in spite of some uncertainties related to the differences in definition among different groups and well-known limitations of the schlieren technique to objectively resolve the spray limit from a background flow [8]. Images in Figure 5 enable the identification of a sharp contour for the reacting case.…”
Section: Figure 3 Tomentioning
confidence: 99%
See 1 more Smart Citation
“…This parameter has been extensively used in many spray studies to characterize the inert spray radial spreading rate [8,25,32,35], in spite of some uncertainties related to the differences in definition among different groups and well-known limitations of the schlieren technique to objectively resolve the spray limit from a background flow [8]. Images in Figure 5 enable the identification of a sharp contour for the reacting case.…”
Section: Figure 3 Tomentioning
confidence: 99%
“…As a result, the combination of HT ambient conditions with 50 MPa injection pressure and small d 0 = 82 m was considered in this section. Although time scales longer than the End Of Injection (EOI) can be visualized for this condition, the analysis presented here is focused on the momentum-driven flame period before EOI rather than on the transient phase after EOI where effects such as entrainment waves [32] occur. Figure 5 show the experimental information that can help identify the different stages on the spray flame transient evolution.…”
Section: Experimental Analysis Of the Transient Flame Penetration Phasesmentioning
confidence: 99%
“…1, the products from the upstream regions of the DF mix with those from the AZ and are convected downstream, where they increasingly dilute the reacting mixtures in the downstream regions of the DF and the jet core. This quasi-steady period continues until injection ends, after which time the last of the liquid fuel vaporizes [27]. Mixing-controlled combustion continues until the majority of the fuel vapor and soot are oxidized or until in-cylinder temperatures drop to sufficiently low values due to gas expansion from piston motion and/or the exhaust valves opening.…”
Section: Introductionmentioning
confidence: 99%
“…This model has been used in literature for complementing studies developed in combustion vessels [24], optical engines [25] and single-cylinder research engines [26]. In 2009, Musculus and Kattke [27] also proposed a 1D model for transient diesel jet with the aim to understand the jet mixing process in case of unsteady injection rate. This was an extension of the Naber and Siebers model and some simplifying assumptions were made based on experimental observations [28].…”
Section: Introductionmentioning
confidence: 99%