Variations of total forces and moments with angles of attack and sideslip, calculated for number of slender plane and cruciform wing-tail combinations under assumption that vortex sheet is fully rolled up ahead of tail.


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    Title :

    Aerodynamic interference of slender wing-tail combinations


    Additional title:

    NACA -- Tech Note


    Contributors:
    Sacks, A.H. (author)


    Publication date :

    1957


    Size :

    81 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :