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Potential of inertial instabilities for fuel film separation in port fuel injection engine conditions
- Source :
- International Journal of Engine Research. 4:11-26
- Publication Year :
- 2003
- Publisher :
- SAGE Publications, 2003.
-
Abstract
- In port fuel injection engines, the liquid fuel film accumulated in the vicinity of intake valves is torn away and goes into the cylinder during the intake phase. In order to predict the fuel mixture preparation inside the cylinder, a model for the fuel film separation near the sharp edges of the intake valves has been developed. A separation criterion is set up using an analogy with Rayleigh-Taylor instabilities driven by the inertial forces of the film. The critical value for the separation criterion is adjusted using experimental data obtained in a two-dimensional wind tunnel fitted with different steps shaped as the valve seat and reproducing the main characteristics of the intake of a spark ignition engine. Computational fluid dynamics simulations are performed using the KMB code, a modified version of KIVA-2 already including a film model and a stochastic Lagrangian description of the spray. Computation for the intake stroke on a four-cylinder 1.9 litre port fuel injection engine confirms that the fuel droplets are not completely vaporized at the end of the intake stroke.
- Subjects :
- Engineering
business.industry
020209 energy
Mechanical Engineering
Aerospace Engineering
Ocean Engineering
02 engineering and technology
Mechanics
Computational fluid dynamics
Automotive engineering
Cylinder (engine)
law.invention
Liquid fuel
Physics::Fluid Dynamics
020303 mechanical engineering & transports
0203 mechanical engineering
law
Valve seat
Spark-ignition engine
Automotive Engineering
0202 electrical engineering, electronic engineering, information engineering
Stroke (engine)
Engine knocking
business
Wind tunnel
Subjects
Details
- ISSN :
- 20413149 and 14680874
- Volume :
- 4
- Database :
- OpenAIRE
- Journal :
- International Journal of Engine Research
- Accession number :
- edsair.doi...........4689a897c3ba2dbd46335c61328f8717
- Full Text :
- https://doi.org/10.1177/146808740300400102