Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk

Experiments are performed on a modern design transonic shroudless low-aspect ratio fan blisk that experienced both subsonic/transonic and supersonic stall-side flutter. High-response flush mounted miniature pressure transducers are utilized to measure the unsteady aerodynamic loading distribution in...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of turbomachinery 2004-01, Vol.126 (1), p.166-174
Hauptverfasser:	Sanders, A. J, Hassan, K. K, Rabe, D. C
Format:	Artikel
Sprache:	eng
Schlagworte:	Applied sciences Continuous cycle engines: steam and gas turbines, jet engines Engines and turbines Exact sciences and technology Mechanical engineering. Machine design
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!