A finite element computational fluids dynamics-based aeroservoelastic analysis methodology is presented in this paper, in which both structural and fluids discretization are achieved by the finite element method, and their interaction is modeled by the transpiration boundary condition technique. In the fluids discipline either inviscid or viscous flow may be accounted for, usually employing unstructured grids. A description of a novel viscous flow solver employing unstructured grids is given in detail. Provisions are made for digital as well as analog controllers. These new aeroservoelastic analysis techniques are next applied for the solution of a number of example problems including the novel Hyper-X launch vehicle. Experimental and actual flight test data are also compared with analysis results that signify to the efficacy and accuracy of the newly developed solution procedures.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computational fluid dynamics-based aeroservoelastic analysis with Hyper-X applications


    Additional title:

    Aeroservoelastische Analyse eines Flugzeugs aus dem Hyper-X-Programm auf Basis numerischer Strömungssimulation


    Contributors:
    Gupta, K.K. (author) / Bach, C. (author)

    Published in:

    AIAA Journal (online) ; 45 , 7 ; 1459-1471


    Publication date :

    2007


    Size :

    13 Seiten, 21 Bilder, 25 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English