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.
Planar Equations of Rollout Motion for an Aircraft with Free or Steerable Landing Gears
1982
54 pages
Report
Keine Angabe
Englisch
Research on Landing and Rollout Dynamic Characteristics of Skid-Equipped Aircraft
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