A method for analyzing the natural vibration characteristics of plate-beam combination structures is presented. Structures of built up delta wings and fuselages are used as examples. Numerical analyses of the aerodynamic characteristics in supersonic flight are developed. Vibration tests were conducted to provide a comparison with the simulation tests. (Author)


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    Title :

    On the Natural Vibration of Plate-Beam Combination Structures, 3


    Contributors:
    T. Hanawa (author) / Y. Hayashi (author) / Y. Tada (author) / S. Toda (author) / K. Kusaka (author)

    Publication date :

    1972


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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