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Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/22008

Title: The impingement characteristics of an early injection GDI engine: a numerical study
Authors: Beavis, Nick J.
Ibrahim, Salah S.
Malalasekera, W.
Issue Date: 2016
Publisher: © The Authors. Published by Sage.
Citation: BEAVIS, N.J., IBRAHIM, S.S. and MALALASEKERA, W., 2016. The impingement characteristics of an early injection GDI engine: a numerical study. International Journal of Engine Research, DOI: 10.1177/1468087416663325
Abstract: This paper describes the use of a Lagrangian discrete droplet model to evaluate the liquid fuel impingement characteristics on the internal surfaces of an early injection gasoline direct injection (GDI) engine. The study focuses on fuel impingement on the intake valve and cylinder liner between start of injection (SOI) and 20° after SOI using both a single- and multi-component fuel. The single-component fuel used was iso-octane and the multi-component fuel contained fractions of iso-pentane, iso-octane and n-decane to represent the light, medium and heavy fuel fractions of gasoline, respectively. A detailed description of the impingement and liquid film modelling approach is also provided Fuel properties, wall surface temperature and droplet Weber number and Laplace number were used to quantify the impingement regime for different fuel fractions and correlated well with the predicted onset of liquid film formation. Evidence of film stripping was seen from the liquid film formed on the side of the intake valve head with subsequent ejected droplets being a likely source of unburned hydrocarbons and particulate matter emissions. Differences in impingement location and subsequent location of liquid film formation were also observed between single- and multi-component fuels. A qualitative comparison with experimental cylinder liner impingement data showed the model to well predict the timing and positioning of the liner fuel impingement.
Description: This is the accepted manuscript version of the paper.
Sponsor: This work was supported by Jaguar Land Rover and the UK-EPSRC grant EP/K014102/1 as part of the jointly funded Programme for Simulation Innovation.
Version: Accepted for publication
DOI: 10.1177/1468087416663325
URI: https://dspace.lboro.ac.uk/2134/22008
Publisher Link: http://dx.doi.org/10.1177/1468087416663325
ISSN: 2041-3149
Appears in Collections:Published Articles (Aeronautical and Automotive Engineering)

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