Method of transfer matrices is used in study of response of flexible airplanes to random vertical gusts; nonhomogeneous and homogeneous gust fields can be treated within present framework; formulation is carried out in case of slender wing with nonuniform sweep angle, which is possible configuration for large supersonic transports; since bending moment, torsional moment, and shear are treated directly as unknowns rather than indirectly obtained from differentiating deflections, method yields more accurate assessment of random stress levels.


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    Titel :

    Transfer matrix representation of flexible airplanes in gust response study


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Lin, Y.K. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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