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A second generation of Common-Rail injection systems is coming into production making feasible multiple injection strategies. This paper aims to assess the capability of multiple injection in reducing NOx and soot emissions of HSDI Diesel engines. The analysis has been carried out at a characteristic point of the EUDC emission test cycle by using a customized version of the CFD code Kiva3, with updated sub-models developed by University of Bologna and University of Wisconsin. In particular, a recent modification has been introduced in the fuel conversion rate calculation in order to account for turbulence non-equilibrium effects. Different multiple injection profiles and combustion chamber configurations have been simulated and their effects on mixture formation, heat release rate and NOx and soot formation have been analyzed. The main target was to comply with emission standards without significant loss in engine performance.

An experimental investigation, using the Laser Doppler Anemometry (LDA) technique, was carried out to investigate the complex structure of the intake flow in a commercial four-cylinder automotive Diesel engine. The attention was focused on the evaluation of the mean motion and turbulence intensity by using a steady state test rig with dynamic valve flow arrangements, supplying a flow rate of 17.4m3/h, that corresponds to the actual flow rate of the engine running at 2,000 rpm. The LDA tests were performed with the engine head mounted on a plexiglas cylinder, having the same diameter as that of the real engine, equipped with optical accesses. The intake manifold was connected to a flow bench tester to simulate the actual flow rates of the engine. Measurement points were located within the cylinder at different distances from the cylinder axis, on two orthogonal diameters, and at different depths from the engine head.

An experimental and numerical investigation, using the Laser Doppler Anemometry (LDA) technique and a 3D fluid-dynamic code (KIVA 3V), was carried out in a prototype engine under steady-state conditions. The aim of the present activity was the flow field characterization and the effect of the intake geometry on the in-cylinder tumble flow. A new steady flow test rig designed for capturing the tumble motion within a test cylinder, made by a blower and an engine head, was assembled to simulate the intake flow. The engine head was mounted on an aluminum cylinder, having the same bore as the real engine. The cylinder was provided with optical accesses on the periphery and a flat optical window located at the bottom to a depth equal to the stroke of the engine. The cylinder was also equipped with two cylindrical ducts, used as air outflow ports.

The paper illustrates an experimental and numerical investigation of the flow generated by an intake port model for a heavy duty direct injection (HDDI) Diesel engine. Tests were carried out on a steady state air flow test rig to evaluate the global fluid-dynamic efficiency of the intake system, made by a swirled and a directed port, in terms of mass flow rate, flow coefficients and swirl number. In addition, because the global coefficients are not able to give flow details, the Laser Doppler Anemometry (LDA) technique was applied to obtain the local distribution of the air velocity within a test cylinder. The steady state air flow rig, made by a blower and the intake port model mounted on a plexiglas cylinder with optical accesses, was assembled to supply the actual intake flow rate of the engine, setting the pressure drop across the intake ports atûP=300 and 500 mm of H2O.

In-cylinder measurements of turbulent integral length scales, carried out during the last 60 degrees of the compression stroke at 600 and 1,000 rpm by a two-probe volume LDV system, were used to assess the capability of the k-ε model used in KIVA-II code. The objective of the paper is to address the following question: what is the most reasonable definition of turbulent length scale in the k-ε model for engine applications? The answer derived from the comparison between KIVA predictions and experiments that showed a fair agreement between the computed turbulent length scale and the measured lateral integral length scale. The agreement is a result of proper choice of the initial swirl ratio and turbulent kinetic energy at inlet valve closure (IVC) by taking into account the LDV measurements and the value of the constant Cμε in the k-ε model equations that relates the turbulent length scale to k and ε.

A customised version of FIRE™ code is chosen to simulate the spray injected into a controlled environment by means of a Common Rail system driven via a Programmable Electronic Control Unit. Numerical results are compared to experimental data collected under various operating conditions, namely varying the injection pressure up to 120 MPa, and the gas back-pressure between 0.1 and 5.0 MPa. Non-evaporating conditions are considered. The employed optically accessible test chamber allows to light the spray with a flash lamp or a pulsed laser sheet, generated on the second harmonic of a Nd-YAG laser (532 nm, 12 ns in duration). Images are collected at different instants of time after the start of injection by means of a CCD camera. A digital image processing software is used to evaluate the major characteristics of the spray, as the penetration length and the cone angle. The injection flow rate is properly measured on a rate-of-injection flow bench for different injection strategies.