Wind tunnel tests of effectiveness of methods of reducing high control forces of unbalanced upper-surface ailerons and of unbalanced split flaps; tests of aileron-axis and flap-axis locations and arrangements of aileron and flap slots, all on Clark Y wing; lift and drag characteristics of various arrangements. (Price 10c.)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind-tunnel investigation of aerodynamic balancing of upper-surface ailerons and split flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1935


    Size :

    18 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :