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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Lifting Surface for Aircraft


    Contributors:
    C. Fauvel (author) / H. Coltel (author)

    Publication date :

    1975


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE

    LLAMAS SANDIN RAUL CARLOS | European Patent Office | 2024

    Free access

    AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE

    LLAMAS SANDIN RAUL CARLOS | European Patent Office | 2024

    Free access

    AIRCRAFT LIFTING SURFACE

    LLAMAS-SANDIN RAUL CARLOS | European Patent Office | 2023

    Free access

    AIRCRAFT LIFTING SURFACE

    MARTINO GONZALEZ ESTEBAN / NOGUEROLES VIÑES PEDRO / RUPEREZ JAVIER | European Patent Office | 2024

    Free access

    AIRCRAFT LIFTING SURFACE

    MARTINO GONZALEZ ESTEBAN / NOGUEROLES VINES PEDRO / RUPEREZ JAVIER | European Patent Office | 2025

    Free access