A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in Sweden and the NASA Langley Research Center regarding the aeroelastic analyses of a full-span fighter configuration wind-tunnel model. This wind-tunnel model was tested in the Transonic Dynamics Tunnel (TDT) in the summer of 2016. Large amounts of data were acquired including steady/unsteady pressures, accelerations, strains, and measured dynamic deformations. The aeroelastic analyses presented include linear aeroelastic analyses, CFD steady analyses, and analyses using CFD-based reduced-order models (ROMs).


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    Title :

    Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data


    Contributors:
    W. A. Silva (author) / P. Chwalowski (author) / C. D. Wieseman (author) / D. Eller (author) / U. Ringertz (author)

    Publication date :

    2017


    Size :

    19 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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