Aeroelastic Stability of Combined Plunge-Pitch Mode Shapes in a Linear Compressor Cascade

Modern aeroengine designs strive for peak specific fuel and thermal efficiency. To achieve these goals, engines have more highly loaded compressor stages, thinner aerofoils, and blended titanium integrated disks (blisks) to reduce weight. These configurations promote the occurrence of aeroelastic ph...

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Bibliographic Details

Published in:	International Journal of Turbomachinery, Propulsion and Power
Main Authors:	George Hill, Julian Gambel, Sabine Schneider, Dieter Peitsch, Sina Stapelfeldt
Format:	Article
Language:	English
Published:	MDPI AG 2022-02-01
Subjects:	flutter aeroelasticity aerodynamic damping linear cascade 1F mode shape
Online Access:	https://www.mdpi.com/2504-186X/7/1/7