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    A Novel Global Optimization Algorithm and Its Application to Airfoil Optimization

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 004::page 41011
    Author:
    Yang, B.
    ,
    Xu, Q.
    ,
    He, L.
    ,
    Zhao, L. H.
    ,
    Gu, Ch. G.
    ,
    Ren, P.
    DOI: 10.1115/1.4028712
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In 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.
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      A Novel Global Optimization Algorithm and Its Application to Airfoil Optimization

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    http://yetl.yabesh.ir/yetl1/handle/yetl/159914
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian