Equations were derived for an aircraft in a three-point attitude. Transient tire forces were simulated by delaying the application of forces derived from steady-state considerations. Predicted rollout trajectories were similar to those measured in tests of a small-scale landing-gear model equipped with pneumatic tires (where a laterally sloping runway was used to simulate a crosswind), both with and without nose-wheel steering.


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    Title :

    Planar equations of rollout motion for an aircraft with free or steerable landing gears


    Contributors:

    Publication date :

    1982-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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