2010
DOI: 10.5293/ijfms.2010.3.2.150
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Multi-objective Optimization of a Laidback Fan Shaped Film-Cooling Hole Using Evolutionary Algorithm

Abstract: Laidback fan shaped film-cooling hole is formulated numerically and optimized with the help of three-dimensional numerical analysis, surrogate methods, and the multi-objective evolutionary algorithm. As Pareto optimal front produces a set of optimal solutions, the trends of objective functions with design variables are predicted by hybrid multi-objective evolutionary algorithm. The problem is defined by four geometric design variables, the injection angle of the hole, the lateral expansion angle of the diffuse… Show more

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Cited by 23 publications
(5 citation statements)
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“…A hybrid multi-objective evolutionary approach is used to obtain the global Pareto-optimal solutions. The methodology that is used to generate the global Pareto-optimal front was reported in the previous works [7,20].…”
Section: Response Surface Approximations and Multi-objective Optimizamentioning
confidence: 99%
“…A hybrid multi-objective evolutionary approach is used to obtain the global Pareto-optimal solutions. The methodology that is used to generate the global Pareto-optimal front was reported in the previous works [7,20].…”
Section: Response Surface Approximations and Multi-objective Optimizamentioning
confidence: 99%
“…Changing and optimizing the geometry parameters of shaped holes is an important method to make the film cooling performance of shaped holes improved. Lee et al [20][21][22] have employed the single objective surrogate model approximation method with the film cooling effectiveness as the objective function to optimize the geometry of fan-shaped holes and laidback fan-shaped holes on the flat surface. Furthermore, they have employed the RSM surrogate model coupling with a multi-objective genetic algorithm to optimize the geometry of laidback fanshaped holes with the film cooling effectiveness and aerodynamic loss as the objective function.…”
Section: Introductionmentioning
confidence: 99%
“…It is of great significance to develop an optimization method for geometric parameters of turbine chamber. Lee et al [8] performed the singleand multiobjective optimization of the fan-shaped hole on the flat plate by using surrogate model method respectively. In the single-objective optimization, maximizing the cooling efficiency was taken as the objective, and the optimized cooling effectiveness increases by 13.5% and 27.8% at the blowing ratio of 0.5 and 1.5, respectively.…”
Section: Introductionmentioning
confidence: 99%