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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    Titel :

    Free wing assembly for an aircraft


    Beteiligte:

    Erscheinungsdatum :

    1978-11-07


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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