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    Computation of Three-Dimensional Nonlinear Panel Flutter

    Source: Journal of Aerospace Engineering:;2003:;Volume ( 016 ):;issue: 004
    Author:
    Raymond E. Gordnier
    ,
    Miguel R. Visbal
    DOI: 10.1061/(ASCE)0893-1321(2003)16:4(155)
    Publisher: American Society of Civil Engineers
    Abstract: A recently developed three-dimensional viscous aeroelastic solver is applied to the solution of nonlinear panel flutter. The solution scheme implicitly couples a well validated Navier-Stokes code with a finite-difference procedure for the Von Karman plate equations by employing a subiteration strategy. Both low supersonic,
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      Computation of Three-Dimensional Nonlinear Panel Flutter

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    https://yetl.yabesh.ir/yetl1/handle/yetl/44991
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    contributor authorRaymond E. Gordnier
    contributor authorMiguel R. Visbal
    date accessioned2017-05-08T21:16:09Z
    date available2017-05-08T21:16:09Z
    date copyrightOctober 2003
    date issued2003
    identifier other%28asce%290893-1321%282003%2916%3A4%28155%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44991
    description abstractA recently developed three-dimensional viscous aeroelastic solver is applied to the solution of nonlinear panel flutter. The solution scheme implicitly couples a well validated Navier-Stokes code with a finite-difference procedure for the Von Karman plate equations by employing a subiteration strategy. Both low supersonic,
    publisherAmerican Society of Civil Engineers
    titleComputation of Three-Dimensional Nonlinear Panel Flutter
    typeJournal Paper
    journal volume16
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2003)16:4(155)
    treeJournal of Aerospace Engineering:;2003:;Volume ( 016 ):;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