Technical study of various systems of braking and of devices for shortening landing runs. Reference is made to investigations by Nat. Advisory Committee for Aeronautics, from which investigations it is concluded that for a given size of propeller, wide blades have a larger brake effect than narrow blades, and that brake effect of higher-pitch propeller is less than that of lower-pitch propeller.


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    Titel :

    Landing run and get-away for standard airplanes


    Weitere Titelangaben:

    J1. Soc. Automotive Engrs


    Beteiligte:


    Erscheinungsdatum :

    1920


    Format / Umfang :

    6 pages


    Anmerkungen:

    9 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    LANDING RUN AND GET-AWAY FOR STANDARD AIRPLANES

    KLEMIN, ALEXANDER | SAE Technical Papers | 1920


    Landing of airplanes

    Philippe | Engineering Index Backfile | 1922


    Landing gears for airplanes

    Maiorca, S. | Engineering Index Backfile | 1930


    Landing speed of airplanes

    Lee, J.G. | Engineering Index Backfile | 1929


    Landing load of airplanes

    Ogawa, T. | Engineering Index Backfile | 1930