Based on the appropriate stiffness and inertial properties of prototypical aircraft landing gear suspension systems, a tire spinup model is developed. Due to its generality, the model can define the various governing dynamical fields. Here the effects of such factors as sink rate, runway friction and aircraft landing speed are considered. Main attention is given to defining the tire deflection-rotation-skidding history as well as the net and pointwise rate of work due to interfacial friction as it effects the growth of rotary inertia and slip work. To quantify the influence of such environmental factor as sink rate, friction and landing speed, a case study involving the shuttle main tires is included.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Landing Induced Tire Spinup


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Kazempour, Amir S. (Autor:in) / Padovan, Joe (Autor:in) / Kim, Tony Hee (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1990



    Erscheinungsdatum :

    01.09.1990




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aircraft landing-induced tire spinup

    PADOVAN, JOE / KAZEMPOUR, AMIR / KIM, YONG H. | AIAA | 1991


    Comparison Between Drop Tower Spindown and Aircraft Spinup Tire Wear

    Macy, Bill / Padovan, Joe / Lay, Megan et al. | SAE Technical Papers | 1995


    Comparison Between Drop Tower Spindown and Aircraft Spinup Tire Wear

    Padovan, J. / Ananthaswamy, V. / Lay, M. et al. | British Library Conference Proceedings | 1995


    Spinup Dynamics of Gyrostats

    Hall, C.D. | Online Contents | 1995


    Spinup dynamics of gyrostats

    Hall, Christopher D. | AIAA | 1995