Hysteresis and bifurcation of flow in fuel injection nozzles

Citation
K. Ramamurthi et al., Hysteresis and bifurcation of flow in fuel injection nozzles, P I MEC E G, 215(G1), 2001, pp. 49-59
Citations number
12
Categorie Soggetti
Aereospace Engineering
Journal title
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
ISSN journal
09544100 → ACNP
Volume
215
Issue
G1
Year of publication
2001
Pages
49 - 59
Database
ISI
SICI code
0954-4100(2001)215:G1<49:HABOFI>2.0.ZU;2-X
Abstract
Separated flows due to cavitation and attached flows with and without cavit ation are investigated for sharp-edged nozzles. The influence of the nozzle diameter, length-diameter ratio and Reynolds number on the bifurcation bet ween the two states of flow is determined. A zone of hysteresis is seen to be present in small sharp-edged nozzles having length-diameter ratios of ab out 1.5-5 owing to a delayed bifurcation from cavitated flow to attached fl ow. The role of nozzle diameters and imperfections in the sharp-edged entry is determined, The onset of separated flows arising from cavitation and su bsequent reattachment due to cessation of cavitation occur at threshold val ues of the cavitation number which vary with the nozzle diameter and the le ngth-diameter ratio. The time for transition from cavitated flow to attache d flow is discussed.