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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    Title :

    Effects of aeroelasticity on stability and control characteristics of airplanes


    Additional title:

    AGARD -- Report


    Contributors:
    Runyan, H.L. (author) / Pratt, K.G. (author) / Bennett, F.V. (author)

    Published in:

    Publication date :

    1961


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :