Description of method developed to estimate percentage of lift carried by airfoil-section fuselage; acceptance by NACA of lift distribution of 25% for airfoil-section fuselage and 75% for wings proposed by M. WATTER in Dec 26 1935 issue, previously indexed. (Supp)


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    Title :

    Lift slope and distribution on Burnelli aeroplanes


    Additional title:

    Flight


    Contributors:
    Klemin, A. (author) / Ruffner, B. (author)

    Published in:

    Flight ; 29 , n 1434 ; p 37-39 + 44


    Publication date :

    1936


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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