Modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for effects of thickness on lift distribution.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for effects of thickness on lift distribution


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Graham, D. (author)


    Publication date :

    1951


    Size :

    17 pages


    Remarks:

    Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :