This paper presents the results of tire footprint studies which were performed to understand the effects of vertical load, camber, yaw, inflation pressure and tire construction on frictional power. Two previously worn F-16 radial and bias tire constructions were selected. All tests were conducted at low speed on a Tire Force Machine having a specialized sensor plate with embedded traction and slip sensors. The tests indicate that the total frictional power for both tire constructions are quite similar at low yaw angles, however, at 4° yaw, the bias tire generated significantly more frictional power than the radial tire.


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    Titel :

    Frictional Power Intensity Measurements for Aircraft Tires


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Atlantic Conference & Exposition ; 1995



    Erscheinungsdatum :

    1995-05-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Frictional Power Intensity Measurements for Aircraft Tires

    Medzorian, J. P. / Chawla, M. D. / SAE | British Library Conference Proceedings | 1995



    Dynamic Properties of Aircraft Tires

    S. K. Clark / R. N. Dodge / G. H. Nybakken | AIAA | 1974


    Airline Experience - Jet Aircraft Tires

    Conner, J. E. | SAE Technical Papers | 1962


    Development of radial aircraft tires

    Olds, R. | Tema Archiv | 1987