An investigation was conducted at the Langley aircraft landing loads and traction facility to determine the cornering characteristics of a 40 x 14-16 type VII aircraft tire. These characteristics, which include the cornering-force and drag-force friction coefficients and self-alining torque, were obtained for the tire operating on dry, damp and flooded runway surfaces over a range of yaw angles from 0 deg to 20 deg and at ground speeds from 5 to 100 knots, both with and without braking. The results of this investigation indicated that the cornering capability of the 40 x 14-16 type VII aircraft tire is degraded by high ground speeds, thin-film lubrication and tire hydroplaning effects on the wet surfaces, and brake torque. The cornering capability is greatly diminished when locked-wheel skids are encountered. (Author)


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    Titel :

    Cornering Characteristics of a 40 by 14-16 Type 7 Aircraft Tire and a Comparison with Characteristics of a C40 by 14-21 Cantilever Aircraft Tire


    Beteiligte:
    J. A. Tanner (Autor:in) / R. C. Dreher (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch