Abstract
T his paper describes a new method for estimating the induction swirl intensity by means of the
numerical simulation of gas flow in the intake port and cylinder to optimize combustion chamber
design.
T h e optimization procedure adopted in the present investigation is based on GENERIC
ALGORITHIMS and allows different fitness functions to be simultaneously maximized. The
parameters to be optimized are related to geometric feature shape of the combustion chamber. The
evaluation phase of GENERIC ALGORITHIMS was performed by simultaneity behavior of each
design with modified version of FLUENT code 6.2.
T he present work represents Direct injection spark ignition engine with different combustion
chamber design to get optimum swirl ratio with different engine speed. The study of the chamber
angle variation is to show the change in air jet value around inlet valves and then design optimum
angle which gets uniform annular jet around each intake valve to give as a result high swirl ratio.
Good results are obtained at engine speed 2500 rpm with pentroof angle 15º for both sides. These
results give good agreement with experimental result by Ref [1], where he used single inlet valve
chamber.
numerical simulation of gas flow in the intake port and cylinder to optimize combustion chamber
design.
T h e optimization procedure adopted in the present investigation is based on GENERIC
ALGORITHIMS and allows different fitness functions to be simultaneously maximized. The
parameters to be optimized are related to geometric feature shape of the combustion chamber. The
evaluation phase of GENERIC ALGORITHIMS was performed by simultaneity behavior of each
design with modified version of FLUENT code 6.2.
T he present work represents Direct injection spark ignition engine with different combustion
chamber design to get optimum swirl ratio with different engine speed. The study of the chamber
angle variation is to show the change in air jet value around inlet valves and then design optimum
angle which gets uniform annular jet around each intake valve to give as a result high swirl ratio.
Good results are obtained at engine speed 2500 rpm with pentroof angle 15º for both sides. These
results give good agreement with experimental result by Ref [1], where he used single inlet valve
chamber.
Keywords
fluid field
internal combustion engines
numerical analysis
swirl intensity