Effects of wing, fuselage, and tail flexibility on stability of motion and effectiveness of control are discussed for various flight conditions including dynamic pressure and Mach number; review of problems, such as reduced roll damping and aileron reversal, and extent to which they appear in recent designs of fighters, bombers, transports; features incorporated to reduce adverse aeroelastic effects on stability and control; results from studies of supersonic transport and winged missile.


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    Titel :

    Effects of aeroelasticity on stability and control characteristics of airplanes


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Runyan, H.L. (Autor:in) / Pratt, K.G. (Autor:in) / Bennett, F.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :