Tests on electromagnetic analogy model simulating thin elliptic wing of aspect ratio 6 in steady roll. (Originally issued as Advance Restricted Report L5F23)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Lifting-surface-theory values of damping in roll and of parameter used in estimating aileron stick forces


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:
    Swanson, S. (author) / Priddy, E.L. (author)


    Publication date :

    1945


    Size :

    33 pages


    Remarks:

    18 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :