Efficiency of two series of propellers having sections with thickness chord ratios of 0.06, 0.08, and 0.10; R.A.F.-6 sections gave about same maximum efficiency as Clark Y propellers and were more efficient for conditions of climb and take-off.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1931


    Size :

    20 pages


    Remarks:

    20 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English