A numerical simulation method was developed and
applied for improving the new direct injection
gasoline engine. The method consists of a spray
wall impingement model, a combustion model based
on the unburnt and burnt gas temperatures and
a solution based local grid refinement technique.
This method was applied for the analysis of the
fan-shaped spray combustion system under late
injection conditions. The following results were
obtained: 1) Almost the same results were obtained
in about one-third the CPU time compared to with
the conventional method, 2) the calculated spray
pattern, mixture formation and combustion processes
are in good agreement with the measurements, and
3) The advantage of the mixture formation of the
fan spray system became clarified. The eddy induced
by the fan spray forms a mixture suitable for
combustion with the least amount of overly lean
mixture.
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