The results of an integrated study of structures, aerodynamics, and controls using the STARS program on two advanced airplane configurations are presented. Results for the X-29A include finite element modeling, free vibration analyses, unsteady aerodynamic calculations, flutter/divergence analyses, and an aeroservoelastic controls analysis. Good correlation is shown between STARS results and various other verified results. The tasks performed on the Oblique Wing Research Aircraft include finite element modeling and free vibration analyses.


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    Title :

    Integrated Study of Structures, Aerodynamics and Controls on the Forward Swept Wing X-29A and the Oblique Wing Research Aircraft


    Contributors:
    K. S. Dawson (author) / P. E. Fortin (author)

    Publication date :

    1987


    Size :

    128 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English