Results of experiments made to determine (1) effect of changing upper and lower camber of thick aerofoils of uniform section, (2) effect of thickening center and thinning tips of thin aerofoil, (3) effect of adding convex lower surface to tapered section, (4) effect of changing mean thickness with constant center and tip sections, and (5) effect of varying chord along span.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The aerodynamic properties of thick aerofoils suitable for internal bracing


    Additional title:

    Nat. Advisory Committee Aeronautics, report



    Publication date :

    1920


    Size :

    26 pages


    Remarks:

    29 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :