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contributor authorYang, B.
contributor authorXu, Q.
contributor authorHe, L.
contributor authorZhao, L. H.
contributor authorGu, Ch. G.
contributor authorRen, P.
date accessioned2017-05-09T01:24:30Z
date available2017-05-09T01:24:30Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_04_041011.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159914
description abstractIn this paper, a novel global optimization algorithm has been developed, which is named as particle swarm optimization combined with particle generator (PSO–PG). In PSO–PG, a PG was introduced to iteratively generate the initial particles for PSO. Based on a series of comparable numerical experiments, it was convinced that the calculation accuracy of the new algorithm as well as its optimization efficiency was greatly improved in comparison with those of the standard PSO. It was also observed that the optimization results obtained from PSO–PG were almost independent of some critical coefficients employed in the algorithm. Additionally, the novel optimization algorithm was adopted in the airfoil optimization. A special fitness function was designed and its elements were carefully selected for the lowvelocity airfoil. To testify the accuracy of the optimization method, the comparative experiments were also carried out to illustrate the difference of the aerodynamic performance between the optimized and its initial airfoil.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Novel Global Optimization Algorithm and Its Application to Airfoil Optimization
typeJournal Paper
journal volume137
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4028712
journal fristpage41011
journal lastpage41011
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 004
contenttypeFulltext


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