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The main objective of the present paper is the application of a detailed kinetic model to study diesel combustion in an optical accessible engine equipped with a common rail injection system. Three different injection schedules made of one to three consecutive injections are considered from both the numerical and the experimental point of view. The numerical model is assessed in such a way to assure its portability with respect to changing injection strategies. The employed detailed kinetic mechanism consists of 305 reactions involving 70 species and is included in the KIVA-3V code. The considered fuel has the liquid phase properties of the diesel oil, the vapor phase properties of C14H28. It is subsequently decomposed into n-heptane and toluene. The chemical solver is based on the use of the reference species technique and on the Partially Stirred Reactor (PaSR) hypothesis. These allow maintaining the computational cost within acceptable limits.

A high swirl divided-chamber Diesel engine system with longitudinal and lateral optical access was developed to study the air-fuel mixing and combustion processes using both conventional and optical techniques. In particular, the spatial and temporal spray evolution, the mixture formation and the combustion phenomena were visualized by a high speed camera. The spatial distribution of soot temperature and soot volume fraction were estimated by spectral flame emissivity measurements using a polychromator with an intensified CCD camera. A modified version of the KIVA-3 numerical code was used to compute the flow field and spray combustion. The code was coupled with a pre-processor to generate the grid of the divided-chamber system and included models of droplet deformation breakup (DDB), single step ignition delay and turbulent mixing-controlled combustion.

Non evaporating diesel sprays from an Electronic Common Rail system are investigated by two different laser light techniques at room temperature within vessels at both ambient and high pressures. Injection is performed by using single-hole injectors of mini-sac type with nozzle orifices 0.18 and 0.22 mm, which operate at injection pressures in the range 40 to 120 MPa. The fuel used is the standard ISO 4113. The densities of ambient gas (nitrogen) are varied in the constant volume vessel within the range 1.2 ÷ 58.4 kg/m3. Two different laser diagnostics are used to infer quantitative information on jet properties. The first is the light Extinction Ratio (ER) method, which is applied at wavelengths 632.8 nm and 832 nm in correspondence of the early instants (∼200÷800 μs) after the end of the liquid injection to infer the average droplet diameter and the number concentration along the line-of-sight. The second experimental technique is the Laser Doppler Anemometry (LDA).