| タイトル | Planar equations of rollout motion for an aircraft with free or steerable landing gears |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820015370 |
| 著者（英） | Sleeper, R. K.; Smith, E. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1982-05-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 82N23244
NASA-TP-1984
L-11689
NAS 1.60:1984 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166134 |
