Critical shimmy speed of nonswiveling landing-gear wheels subject to lateral loading
The paper presents a nonlinear model describing vibration of the landing gear relative to the fuselage. The model is intended to analyze the dynamic stability of nonswiveling main-gear wheels. The model is used to show that the lateral component of the fuselage speed has a significant effect on the...
Gespeichert in:
| Veröffentlicht in: | International applied mechanics 2006-09, Vol.42 (9), p.1077-1084 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | The paper presents a nonlinear model describing vibration of the landing gear relative to the fuselage. The model is intended to analyze the dynamic stability of nonswiveling main-gear wheels. The model is used to show that the lateral component of the fuselage speed has a significant effect on the critical shimmy speed |
|---|---|
| ISSN: | 1063-7095 1573-8582 |
| DOI: | 10.1007/s10778-006-0179-8 |