The chart accompanying this note refers to symmetrical aerofoils of the N.A.C.A. family, but the ordinary magnitude of the mean camber will have no practical influence on the results if it is also used for non-symmetrical aerofoils.


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    Title :

    Aerofoil Sections and Torsion


    Subtitle :

    Geometrical Properties of Symmetrical N.A.C.A. Aerofoils for use in Torsional Calculations


    Contributors:
    David, F. (author)


    Publication date :

    1940-02-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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