The
Homogeneous Charge Compression Ignition (HCCI) combustion concept
is currently under widespread investigation due to its potential
to increase thermal efficiency while greatly decreasing harmful
exhaust pollutants. Simulation tools have been developed to explore
the implications of initial mixture thermodynamic state on engine
performance and emissions. In most cases these modeling efforts
have coupled a detailed fuel chemistry mechanism with empirical
descriptions of the in-cylinder heat transfer processes. The primary
objective of this paper is to present a fundamentally based boundary
layer heat transfer model. The two-zone combustion model couples
an adiabatic core zone with a boundary layer heat transfer model.
The model predicts film coefficient, with approximately the same
universal shape and magnitudes as an existing global model. In
addition, the new model resolves the boundary layer thickness
and mass fraction trapped in the boundary layer, which are needed
to predict and understand hydrocarbon quench. The two-zone model
is then validated against experimental data and compared to the
single zone formulation, which utilizes empirical heat transfer
treatments. |