Rules that must be followed in order to secure longitudinal stability and controllability and safety against stall in tail-first or Canard type airplane are determined for both conditions of power-off and power-on, whether high lift devices are operating or not; procedures for selection or determination of airfoil section, aspect ratio and area of tail surface, tail length and angle of setting of stabilizer are indicated.


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    Title :

    Proportioning "Canard" airplane for longitudinal stability and safety against stall


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Foa, J.V. (author)


    Publication date :

    1942


    Size :

    6 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






    Canard type light personal airplane

    Raynes, B.F. | Engineering Index Backfile | 1946


    Canard type light personal airplane

    Raynes, B.F. | Engineering Index Backfile | 1946