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Planar equations of rollout motion for an aircraft with free or steerable landing gears
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sleeper, R. K. Smith, E. G. |
| Copyright Year | 1982 |
| Description | 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. |
| File Size | 2323872 |
| Page Count | 55 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820015370 |
| Archival Resource Key | ark:/13960/t4jm7399b |
| Language | English |
| Publisher Date | 1982-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Rolling Contact Loads Aircraft Landing Ground Wind Landing Gear Aircraft Tires Roll Equations of Motion Pneumatic Equipment Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
