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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    Titel :

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


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Foa, J.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1942


    Format / Umfang :

    6 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Canard type light personal airplane

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


    Canard type light personal airplane

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