Simple method suggested for design of wings whose aerodynamic center is independent of variation of lateral dimensions of wing; method applied to tapered wings, and good agreement found with tests on wings with straight trailing edges, and taper ratio of 0.303.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Note on position of aerodynamic center of pointed wings at subsonic speeds


    Additional title:

    Stockholm. Kungl. Tekniska Hogskolan -- Inst Flygteknik -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :