Tests made on model of airplane with zero stagger, fairly small gap-chord ratio, and round-section fuselage; and wind-channel tests of pitching and yawing moments with sideslip made with a view to finding any reasons why it should be difficult to bring airplane of this type out of a spin.


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    Title :

    Pitching and yawing moments with sideslip on a model aeroplane with zero stagger


    Additional title:

    Aeronautical Research Committee -- Reports Memoranda


    Contributors:


    Publication date :

    1925


    Size :

    14 pages


    Remarks:

    15 Figs. on supp. plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :