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:
    R. K. Sleeper (author) / E. G. Smith (author)

    Publication date :

    1982


    Size :

    54 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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