A computational procedure is presented for evaluating the analytic sensitivity derivatives of the tire response with respect to material and geometrical properties of the tire. The tire is modeled by using a two-dimensional laminated anisotropic shell theory with the effects of variation in material and geometric parameters included. The computational procedure is applied to the case of the Space Shuttle orbiter nose-gear tire subjected to uniform inflation pressure. Numerical results are presented which show the sensitivity of the different tire response quantities to variations in the material characteristics of both the cord and rubber.


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    Titel :

    Analytical studies of the Space Shuttle orbiter nose-gear tire


    Beteiligte:

    Erscheinungsdatum :

    01.04.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Analytical Studies of the Space Shuttle Orbiter Nose-Gear Tire

    Noor, Ahmed K. / Peters, Jeanne M. / Tanner, John A. et al. | SAE Technical Papers | 1991



    Cornering and Wear Characteristics of the Space Shuttle Orbiter Nose-Gear Tire

    Davis, Pamela A. / Stubbs, Sandy M. / Vogler, William A. | SAE Technical Papers | 1989


    Cornering and wear characteristics of the Space Shuttle Orbiter nose-gear tire

    Davis, Pamela A. / Stubbs, Sandy M. / Vogler, William A. | NTRS | 1989


    Cornering and wear characteristics of the Space Shuttle Orbiter nose-gear tire

    Davis, P.A. / Stubbs, S.M. / Vogler, W.A. | Tema Archiv | 1989