Influence of weak and strong gyroscopic effects on light aircraft dynamics

Purpose The purpose of this study is to investigate the influence of gyroscopic effects on the dynamic stability and the response of light aircraft to manoeuvres following either a rapid deflection of the control surfaces or wind gust. Design/methodology/approach The analyses were conducted for seve...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Aircraft engineering 2016-09, Vol.88 (5), p.613-622
Hauptverfasser:	Goraj, Zdobyslaw Jan, Cichocka, Ewa
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aircraft accidents & safety Aircraft design Aircraft stability Aviation Control surfaces Design Dynamic stability Eigenvalues Energy consumption Equations of motion Flight tests Gas turbine engines General aviation Inertia Light aircraft Linear equations Maneuvers Mathematical models Measurement methods Model testing Nonlinear equations Nonlinear response Parameter sensitivity Velocity Wind tunnel testing Wind tunnels
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!