Simple procedure results in more accurate span loadings, lift curve slopes, and spanwise centers of pressure being read directly from charts of NACA Report 921, indexed in Engineering Index 1951 p 45.


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    Title :

    Correction of additional span loadings computed by WEISSINGER seven-point method for moderately tapered wings of high aspect ratio


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1955


    Size :

    31 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :