YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Optimization of Rotating Blades with Dynamic‐Behavior Constraints

    Source: Journal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 002
    Author:
    Ting Nung Shiau
    ,
    S. J. Chang
    DOI: 10.1061/(ASCE)0893-1321(1991)4:2(127)
    Publisher: American Society of Civil Engineers
    Abstract: The optimal design of rotating pretwisted blades subject to dynamic behavior constraints is studied. The restrictions on multiple blade natural frequencies and on maximum blade dynamic deflections are considered the dynamic behavior constraints. The aerodynamic forces acting on the rotating blades are simulated as harmonic excitations. Optimization techniques of the optimality‐criterion method and the method of modified feasible directions have been successfully developed and applied to minimize the weight of rotating pretwisted blades. Based on these techniques, the numerical results show that the effect of setting angle on the optimal design weight for the first frequency‐constraint case is more significant than that for the second frequency‐constraint case. It is also shown that the changes of pretwist angle will considerably affect the optimal design weight for the second frequency‐constraint case. However the effect is not significant for the fundamental frequency‐constraint case. The results also indicate that the increase of rotating speed will decrease the optimal design weight.
    • Download: (792.5Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Optimization of Rotating Blades with Dynamic‐Behavior Constraints

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/44701
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorTing Nung Shiau
    contributor authorS. J. Chang
    date accessioned2017-05-08T21:15:38Z
    date available2017-05-08T21:15:38Z
    date copyrightApril 1991
    date issued1991
    identifier other%28asce%290893-1321%281991%294%3A2%28127%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44701
    description abstractThe optimal design of rotating pretwisted blades subject to dynamic behavior constraints is studied. The restrictions on multiple blade natural frequencies and on maximum blade dynamic deflections are considered the dynamic behavior constraints. The aerodynamic forces acting on the rotating blades are simulated as harmonic excitations. Optimization techniques of the optimality‐criterion method and the method of modified feasible directions have been successfully developed and applied to minimize the weight of rotating pretwisted blades. Based on these techniques, the numerical results show that the effect of setting angle on the optimal design weight for the first frequency‐constraint case is more significant than that for the second frequency‐constraint case. It is also shown that the changes of pretwist angle will considerably affect the optimal design weight for the second frequency‐constraint case. However the effect is not significant for the fundamental frequency‐constraint case. The results also indicate that the increase of rotating speed will decrease the optimal design weight.
    publisherAmerican Society of Civil Engineers
    titleOptimization of Rotating Blades with Dynamic‐Behavior Constraints
    typeJournal Paper
    journal volume4
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1991)4:2(127)
    treeJournal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian