Model of hypothetical canard airplane, designed to be of same size and general aerodynamic characteristics as Boeing B-247 airplane, was tested in NACA gust tunnel at one wind loading, one forward speed, one gust velocity, and three gust gradients; results of tests presented and discussed.


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    Title :

    Measurements and analysis of motion of canard airplane model in gusts


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Donely, P. (author) / Pierce, H.B. (author) / Pepoon, P.W. (author)


    Publication date :

    1940


    Size :

    20 pages


    Remarks:

    9 Supp Sheets, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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