Analysis is made by means of equations of motions with aircraft pitch and fundamental wing bending degrees of freedom; possibility of employing technique of large concentrated masses at wing tips in nuclear or military aircraft.


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    Title :

    Effects of large wing-tip masses on oscillatory stability of wing bending coupled with airplane pitch


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Airplane wing

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