The braking and cornering response of a slip velocity controlled, pressure bias modulated aircraft antiskid braking system is investigated. The investigation, conducted on dry and wet runway surfaces, utilized one main gear wheel, brake, and tire assembly of a McDonnell Douglas DC 9 series 10 airplane. The landing gear strut was replaced by a dynamometer. The parameters, which were varied, included the carriage speed, tire loading, yaw angle, tire tread condition, brake system operating pressure, and runway wetness conditions. The effects of each of these parameters on the behavior of the skid control system is presented. Comparisons between data obtained with the skid control system and data obtained from single cycle braking tests without antiskid protection are examined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Behavior of Aircraft Antiskid Braking Systems on Dry and Wet Runway Surfaces. A Slip-Velocity-Controlled, Pressure-Bias-Modulated System


    Beteiligte:
    S. M. Stubbs (Autor:in) / J. A. Tanner (Autor:in) / E. G. Smith (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    194 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch