Presentation of method developed by author for rapidly varying airplane drag without disturbing aerodynamic qualities necessary for optimum control at lesser velocities such as employed during alighting; it is suggested that small auto-rotating rotor be installed at craft's tail to produce aerodynamic drag.


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    Titel :

    Rotative flight brake proposed to moderate landing speeds


    Weitere Titelangaben:

    Aviation


    Beteiligte:
    Ray, J.G. (Autor:in)

    Erschienen in:

    Aviation ; 46 , n 1


    Erscheinungsdatum :

    1947


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Landing Speeds

    Swatton, P. J. | Wiley | 2000



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    Devices for reducing landing speeds

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