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The effect of auxiliary gas injection on diesel engine combustion and emissions was studied using KIVA, a multidimensional computational fluid dynamics code. Auxiliary gas injection (AGI) is the injection of gas, in addition to the fuel injection, directly into the combustion chamber of a diesel engine. The objective of AGI is to influence the diesel combustion via mixing to reduce the emissions of pollutants (soot and NOx). In this study, the accuracy of modeling high-speed gas jets on very coarse computational grids was addressed. KIVA was found to inaccurately resolve jet flows near walls. The cause of this inaccuracy was traced to the RNG k - ϵ turbulence model with the law-of-the-wall boundary condition used by KIVA. By prescribing the length scale near the nozzle exit, excellent agreement between computed and theoretical jet penetration was obtained for a transient jet into a quiescent chamber at various operating conditions.

A modification of the computational fluid dynamics code KIVA-II is presented that allows computations to be made in complex engine geometries. An example application is given in which three versions of KIVA-II are run simultaneously. Each version considers a separate block of the computational domain, and the blocks exchange boundary condition information with each other at their common interfaces. The use of separate blocks permits the connectedness of the overall computational domain to change with time. The scavenging flow in the cylinder, transfer pipes (ports), and exhaust pipe of a ported two-stroke engine with a moving piston was modeled in this way. Results are presented for three engine designs that differ only in the angle of their boost ports. The calculated flow fields and the resulting fuel distributions are shown to be markedly different with the different geometries.