Influence of Wing and Fuselage on Vertical-Tail Contribution to Low-Speed Rolling Derivatives of Midwing Airplane Models with 45° Sweptback Surfaces.


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    Title :

    Influence of wing and fuselage on vertical-tail contribution to low-speed rolling derivatives of midwing airplane models with 45° sweptback surfaces


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1951


    Size :

    55 pages


    Remarks:

    Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :