Improving fuel–air mixing remains a critical pathway for reducing emissions and enhancing efficiency in compression-ignition (CI) diesel engines, particularly under increasingly stringent environmental regulations. In-cylinder flow organization, governed primarily by piston bowl geometry and swirl ratio (SR), plays a decisive role in spray development, turbulence generation, and mixture preparation prior to ignition. Despite extensive prior research, the combined influence of multiple piston bowl geometries and swirl intensities under identical, non-reacting conditions has not been systematically quantified. In this study, a comprehensive numerical investigation is conducted to examine the coupled effects of piston bowl geometry and initial swirl ratio on in-cylinder flow evolution, spray dynamics, and fuel–air mixing under motored conditions. Four representative piston bowl geometries of ω-shaped, re-entrant, semi-ellipsoid, and double-swirl are analyzed using a validated Eulerian–Lagrangian CFD framework with the RNG k–ε turbulence model. All configurations are evaluated under equal bowl volume, compression ratio, and injection conditions, with initial SR varied from 0 to 3 to isolate aerodynamic effects from combustion chemistry.
The results reveal strong geometry-dependent swirl amplification and turbulence evolution near top dead center. The semi-ellipsoid bowl achieves the highest swirl amplification (up to ∼78%) and evaporation fraction (∼18%), owing to reduced shear losses and enhanced rotational preservation. The double-swirl geometry promotes distributed turbulence and minimizes wall impingement through flow partitioning, while the re-entrant bowl prioritizes turbulence generation at the expense of swirl amplification. Across all geometries, increasing SR reduces axial spray penetration (up to ∼8%) while enhancing lateral dispersion. To quantitatively assess mixture formation, a new effective penetration metric (combining axial penetration and lateral spread) is introduced. This metric demonstrates that moderate swirl levels (SR ≈ 2) maximize usable mixing volume (32–36 mm) for all geometries. Excessive swirl leads to jet distortion, plume interaction, and reduced chamber utilization. Overall, this work provides a unified, quantitative framework for evaluating bowl–swirl interactions and delivers practical design guidelines for advanced diesel combustion chambers, supporting cleaner and more efficient engine operation in next-generation applications.
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