Aeroelastic analysis is performed on a parallel computer using Euler equations coupled with an advanced wing-box structural model. The wing-box consists of a 3-noded triangular element, with two inplane translations and an in-plane rotation at each node, and axial rods. The 9 degree of freedom triangular element provides more accurate stress analysis than previous studies. A typical wing-body configuration is chosen for the analysis with the assumption of a rigid body. Preliminary results are presented.


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    Title :

    Parallel aeroelastic computation by using coupled Euler flow and wing-box structural models


    Additional title:

    Parallele Aeroelastizitätsberechnung unter Verwendung der Eulerschen Strömungsgleichungen, gekoppelt mit einem Flügelkasten-Strukturmodell


    Contributors:
    Bhardwaj, M.K. (author) / Kapania, R.K. (author) / Byun, C. (author) / Guruswamy, G.P. (author)


    Publication date :

    1995


    Size :

    3 Seiten, 6 Bilder, 9 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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