A method to compute sensitivities for use in gradient-based shape optimization applied to unsteady aeroelasticity problems is presented. The method takes into account the coupling between all three fundamental aspects of computational aeroelasticity: namely, unsteady flow equations, time-varying structural response to aerodynamic loads, and dynamic meshes that accommodate geometric deformations. The devised method provides discretely exact sensitivities of time-integrated and non-time-integrated objective functions with respect to design variables that control the shape of geometry. The algorithm is formulated in a general manner and can be readily extended to coupled multidisciplinary problems involving any number of disciplines. The algorithm is applied to a simple two-dimensional flutter model to demonstrate the proof of concept.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Adjoint-based sensitivity formulation for fully coupled unsteady aeroelasticity problems


    Weitere Titelangaben:

    Adjungiert-basierte Sensitivitätsformulierung für vollständig instationäre Aeroelastizitätsprobleme


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 47 , 8 ; 1902-1915


    Erscheinungsdatum :

    2009


    Format / Umfang :

    14 Seiten, 19 Bilder, 1 Tabelle, 31 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch