An approximate formula is derived for the position of the neutral point in canard aircraft. This formula accounts for the aerodynamic interference between the wing (rear wing) and the canard (forward wing). Topics covered include determination of the canard downwash derivative, determination of the canard and wing liftslopes including the aerodynamic interference, and calculation of the neutral point position.


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    Title :

    Approximate neutral point of a subsonic canard aircraft


    Contributors:

    Publication date :

    1985-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :





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