A free wing is attached to a fuselage of an aircraft in a manner such that the wing is free to pivot about a spanwise axis forward of its aerodynamic center. The wing is angularly displaced about the axis by aerodynamic pitching moments, resulting from lift, and is trimmed through a use of a trimmable free stabilizer comprising a floating canard mounted on a strut rigidly connected to the wing and projected forward from it.


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    Title :

    Free wing assembly for an aircraft


    Contributors:

    Publication date :

    1978-11-07


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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