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    The Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002::page 256
    Author:
    N. L. Sanger
    DOI: 10.1115/1.3227410
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method is presented for automating compressor blade design using numerical optimization and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization procedure is employed, which is based on conjugate directions for locally unconstrained problems and on feasible directions for locally constrained problems. Coupled to the optimizer is an analysis package consisting of three analysis programs which calculate blade geometry, inviscid flow, and blade surface boundary layers. The optimization concepts are briefly discussed. Selection of design of a two-dimensional blade section is discussed, and design results are presented.
    keyword(s): Design , Optimization , Diffusion (Physics) , Compressors , Blades , Geometry , Stators , Inviscid flow AND Boundary layers ,
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      The Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97093
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorN. L. Sanger
    date accessioned2017-05-08T23:15:32Z
    date available2017-05-08T23:15:32Z
    date copyrightApril, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26781#256_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97093
    description abstractA method is presented for automating compressor blade design using numerical optimization and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization procedure is employed, which is based on conjugate directions for locally unconstrained problems and on feasible directions for locally constrained problems. Coupled to the optimizer is an analysis package consisting of three analysis programs which calculate blade geometry, inviscid flow, and blade surface boundary layers. The optimization concepts are briefly discussed. Selection of design of a two-dimensional blade section is discussed, and design results are presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading
    typeJournal Paper
    journal volume105
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227410
    journal fristpage256
    journal lastpage264
    identifier eissn0742-4795
    keywordsDesign
    keywordsOptimization
    keywordsDiffusion (Physics)
    keywordsCompressors
    keywordsBlades
    keywordsGeometry
    keywordsStators
    keywordsInviscid flow AND Boundary layers
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
    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
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