2014
DOI: 10.1016/j.egypro.2014.01.076
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A Numerical Methodology for the Multi-objective Optimization of the DI Diesel Engine Combustion

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Cited by 31 publications
(12 citation statements)
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“…Once the simulations have been validated, any number of parameters can be modified and readily tested. This encouraged development of additional techniques for the identification of optimization pathways with respect to combustion chamber design [25] or engine operating conditions [26,27]. The interest in optimization methods based on genetic algorithm (GA) has increased in the automotive industry over the last few years due to the wide range of solutions they offer in combination with CFD.…”
mentioning
confidence: 99%
“…Once the simulations have been validated, any number of parameters can be modified and readily tested. This encouraged development of additional techniques for the identification of optimization pathways with respect to combustion chamber design [25] or engine operating conditions [26,27]. The interest in optimization methods based on genetic algorithm (GA) has increased in the automotive industry over the last few years due to the wide range of solutions they offer in combination with CFD.…”
mentioning
confidence: 99%
“…As it was reported in the literature, the swirl in diesel engines is an important parameter that affects the mixing rate of air and fuel, heat release rate, emissions, and overall engine performance (Costa et al, 2014). It also observed that there is an optimum level of swirl for particular combustion chamber geometry.…”
Section: Introductionmentioning
confidence: 63%
“…According to the constraint conditions, each design variable is geometric parameters of planar mechanism, so it must meets the requirements of planar mechanism freedom movement and at the same time the basic requirements of pantograph work. Scope of every design variable which can be concluded as follows: This article is from the pantograph structure parameters to study the equivalent mass, so the formula of equivalent mass can be further simplified as: (10) In order to further obtain the optimal value of equivalent mass, combined with the budget law, again from the impact factors to consider, get the following formula: (11) Combined with operation boundary condition, according to the above mathematical model, applying the optimization toolbox of MATLAB language programming, the optimization results are worked out. In which large values: d, L 4 , L 2 , ã, smaller values: a, b, k, L 3 .…”
Section: Matlab Optimization Methodsmentioning
confidence: 99%
“…From the previous formula, the trajectories of rising pantograph and equivalent mass are decided by the design variables. So this is a multi-objective optimization problem [9,10].…”
Section: The Constraint Conditionsmentioning
confidence: 99%