Study made in transonic Ames wind tunnel to investigate effectiveness of tail; lift, drag, and pitching moment coefficients are determined and effective downwash characteristics at tail evaluated and presented.


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    Title :

    Effectiveness of all-movable horizontal tail on unswept-wing and body combination for mach numbers from 0.60 to 1.40


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :