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
1982-05-01
Report
No indication
English
Research on Landing and Rollout Dynamic Characteristics of Skid-Equipped Aircraft
Springer Verlag | 2024
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