Effect of System Mode and Structural Damping Perturbation on the Mistuned Forced Response and Aerodynamic Damping of Embedded Compressor Rotors

This paper is a continuation of previous papers by the authors that focuses on predicting the mistuned embedded rotor blade forced response. The compressor under consideration is a part of a 3.5stage rig located at Purdue University. Previously, the current authors have discussed the impact of sideb...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of engineering for gas turbines and power 2023-05, Vol.145 (5)
Hauptverfasser:	Hegde, Shreyas, Inge, Jonathan D., Kielb, Robert
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!