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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rotative flight brake proposed to moderate landing speeds


    Additional title:

    Aviation


    Contributors:
    Ray, J.G. (author)

    Published in:

    Aviation ; 46 , n 1


    Publication date :

    1947


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Landing Speeds

    Swatton, P. J. | Wiley | 2000



    COMMANDE DE DEVERROUILLAGE ROTATIVE

    ROUSSEAU XAVIER / ABREU XAVIER | European Patent Office | 2016

    Free access

    New instrument system proposed for flight and landing safety

    Jackson, H.L. | Engineering Index Backfile | 1947


    Devices for reducing landing speeds

    Berger, P. | Engineering Index Backfile | 1930