Loughborough University
Leicestershire, UK
LE11 3TU
+44 (0)1509 263171
Loughborough University

Loughborough University Institutional Repository

Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/8412

Title: A CFD model with optical validation on in-cylinder charge performances of CAI engines
Authors: Osei-Owusu, Paul
Chen, Rui
Ibrahim, Salah S.
Wigley, Graham
Patel, Samir N.D.H.
Picher, Graham
Keywords: Air-fuel ratio
Anemometers
Autoignition
Computational fluid dynamics
Diesel engines
Engine tests
Ignition timing
Lasers
Mathematical models
Mesh generation
Optical equipment
Pressure
Research and development
Single cylinder engines
Temperature
Issue Date: 2008
Publisher: © SAE International
Citation: OSEI-OWUSU, P. ... et al, 2008. A CFD model with optical validation on in-cylinder charge performances of CAI engines. IN: Proceedings of SAE 2008 World Congress, Detroit, Michigan, 14th-17th April.
Series/Report no.: SAE International;2008-01-0045
Abstract: Over the past few decades, Homogeneous Charge Compression Ignition (HCCI) or Controlled Auto-Ignition (CAI) if it is fuelled with gasoline type of fuels has shown its potential to overcome the limitations and environmental issue concerns of the Spark Ignition (SI) and Compression Ignition (CI) engines. However, controlling the ignition timing of a CAI engine over a wide range of speeds and loads is challenging. Combustion in CAI is affected by a number of factors; the local temperature, the local composition of the air/fuel mixture, time and to a lesser degree the pressure. The in-cylinder engine charge flow fields have significant influences on these factors, especially the local gas properties, which leads to the influences towards the CAI combustion. In this study, such influences were investigated using a Computational Fluid Dynamics (CFD) engine simulation package fitted with a real optical research engine geometry. Applying a Laser Doppler Anemometry (LDA) to the same engine, the cycle averaged time history mean and Root Mean Square (RMS) velocity profiles for the axial and radial velocity components in three axial planes were measured throughout the inlet and compression stroke. The calculated results were compared with the experimental results in terms of the vectors flow fields, averaged integrated tumble ratio as a function of crankangle and the local velocities in this paper. The results from both studies showed good correlations.
Description: This is a conference paper [2008 © SAE International]. It was posted on this site with permission from SAE International. Further use and distribution of this paper requires permission from SAE International.
Version: Published
URI: https://dspace.lboro.ac.uk/2134/8412
Publisher Link: http://www.sae.org/congress/2008/
ISSN: 0148-7191
Appears in Collections:Conference Papers and Contributions (Aeronautical and Automotive Engineering)

Files associated with this item:

File Description SizeFormat
DownloadComponent[1].pdf2.31 MBAdobe PDFView/Open

 

SFX Query

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.