Investigation of Effects of Leading-Edge Chord-Extensions and Fences in Combination with Leading-Edge Flaps on Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of 45° Sweptback Wing of Aspect Ratio 4.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on aerodynamic characteristics at mach numbers from 0.40 to 0.93 of 45° sweptback wing of aspect ratio 4


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1957


    Size :

    45 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :