A pre-World War 2 German patent is described for an airplane wing whose profile is automatically changed as a function of the flight parameters (velocity, angle of attack, etc.) in such a manner that the center of pressure always remains approximately at the same place. The patent includes an automatic steering device for aircraft. Conventional and wing-only aircraft are considered. (Author)


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    Titel :

    Lifting Surface for Aircraft


    Beteiligte:
    C. Fauvel (Autor:in) / H. Coltel (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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