Theoretical Analysis of Effect of Aileron Inertia and Hinge Moment on Maximum Rolling Acceleration of Airplanes in Abrupt Aileron Rolls. (Advance Restricted Report Feb 1942)


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    Title :

    Theoretical analysis of effect of aileron inertia and hinge moment on maximum rolling acceleration of airplanes in abrupt aileron rolls


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1942


    Size :

    13 pages


    Remarks:

    3 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :