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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Analytical studies of the Space Shuttle orbiter nose-gear tire


    Contributors:

    Publication date :

    1991-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    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 Archive | 1989