Method is developed for determining twist of swept-back wing with prescribed spanwise lift distribution; explicit formulas are derived for case that lift is given at eight points of semi-span. (see also - n 8 (discussion) Oct p 320-1)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Influence of sweep on spanwise lift distribution of wings


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1943


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :