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Journal Article

Alternative Diesel Fuels Characterization in Non-Evaporating and Evaporating Conditions for Diesel Engines

2010-05-05
2010-01-1516
This paper reports the study of the effects of alternative diesel fuel and the impact for the air-fuel mixture preparation. The injection process characterization has been carried out in a non-evaporative high-density environment in order to measure the fuel injection rate and the spatial and temporal distribution of the fuel. The injection and vaporization processes have been characterized in an optically accessible single cylinder Common Rail diesel engine representing evaporative conditions similar to the real engine. The tests have been performed by means of a Bosch second generation common rail solenoid-driven fuel injection system with a 7-holes nozzle, flow number 440 cc/30s @100bar, 148deg cone opening angle (minisac type). Double injection strategy (pilot+main) has been implemented on the ECUs corresponding to operative running conditions of the commercial EURO 5 diesel engine.
Technical Paper

Evaluation of Splash Models with High-Pressure Diesel Spray

2006-04-03
2006-01-1117
Spray impingement on walls is an important physical process in modern DI Diesel engines as it greatly influences mixture formation, combustion process and exhaust emissions. The mixture preparation is, in fact, a crucial aspect for the correct operation of the engine as it significantly affects the combustion process. In this paper three models, among the available in literature, have been selected and implemented in the KIVA-3V code. Namely, the models by O'Rourke and Amsden (OA model) [1, 2], by Bai and Gosman (BG model) [3] and by Lee et al. (LR model) [4, 5] are compared in terms of performance and capability of representing the splash phenomenon. The model capabilities are firstly tested comparing the numerical results with four sets of experimental literature data, characterized by low injection pressures. The high injection pressures of modern Diesel engines result in droplets velocities emerging from the nozzle greater than 300 m/s.
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