AIRCRAFT DYNAMICS DURING FLIGHT IN ICING CONDITIONS

This paper presents numerical analysis of airplane motion parameters during wing in-flight icing. The wing external flaps deflection event was taken under consideration. The mathematical model of the airplane motion including twelve ordinary differential equations was employed. Using available publi...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of Theoretical and Applied Mechanics (Warsaw) 2012-01, Vol.50 (1), p.269-284
Hauptverfasser:	Kowaleczko, Grzegorz, Wachlaczenko, Michal
Format:	Artikel
Sprache:	eng
Schlagworte:	Airplanes Computer programs Differential equations Dynamic tests Dynamics Icing Mathematical models Wings (aircraft)
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!