2013
DOI: 10.1155/2013/275091
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Framework for the Shape Optimization of Aerodynamic Profiles Using Genetic Algorithms

Abstract: This study developed a framework for the shape optimization of aerodynamics profiles using computational fluid dynamics (CFD) and genetic algorithms. A genetic algorithm code and a commercial CFD code were integrated to develop a CFD shape optimization tool. The results obtained demonstrated the effectiveness of the developed tool. The shape optimization of airfoils was studied using different strategies to demonstrate the capacity of this tool with different GA parameter combinations.

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Cited by 6 publications
(3 citation statements)
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“…Similar application papers have also applied GA to computational fluid dynamics. 28,29 Alternative methods to GAs have also been proposed, to a lesser extent, such as sequential approximation optimization, 30 evolutionary strategies, 31,32 DE, 33 PSO, 34 harmony search, 35 and EDAs. 36 The use of local optimization methods has also been referred in the literature, being simulated annealing (SA) 37,38 one of the most common approaches, but other approaches such as VNS 39 and TS 40 have also been considered.…”
Section: Related Workmentioning
confidence: 99%
See 1 more Smart Citation
“…Similar application papers have also applied GA to computational fluid dynamics. 28,29 Alternative methods to GAs have also been proposed, to a lesser extent, such as sequential approximation optimization, 30 evolutionary strategies, 31,32 DE, 33 PSO, 34 harmony search, 35 and EDAs. 36 The use of local optimization methods has also been referred in the literature, being simulated annealing (SA) 37,38 one of the most common approaches, but other approaches such as VNS 39 and TS 40 have also been considered.…”
Section: Related Workmentioning
confidence: 99%
“…In particular, Corriveau et al applied GA to optimize FEM, for benchmark use cases and to a real‐case scenario of fillets at the crown‐blade junctions of a hydroelectric turbine. Similar application papers have also applied GA to computational fluid dynamics …”
Section: Related Workmentioning
confidence: 99%
“…The damage location is formulated as a constrained optimization problem and solved using the DE algorithm based on the measured and calculated first three natural frequencies as inputs. A framework for the shape optimization of aerodynamics profiles using computational fluid dynamics and genetic algorithms proposed by López et al [ 9 ]. A DE optimization based technique is proposed to find the optimum value of a modified Bezier curve.…”
Section: Introductionmentioning
confidence: 99%