On the Interaction of Multiple Traveling Wave Modes in the Flutter Vibrations of Friction-Damped Tuned Bladed Disks
Author:
Affiliation:
1. Institute of Aircraft Propulsion Systems, University of Stuttgart, Stuttgart 70569, Germany e-mail:
2. Institute of Dynamics and Vibration Research, Leibniz Universität Hannover, Hannover 30167, Germany e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4034650/6173518/gtp_139_04_042501.pdf
Reference19 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades;ASME J. Eng. Gas Turbines Power,1997
2. A Review of Aeroelasticity Methods With Emphasis on Turbomachinery Applications;J. Fluids Struct.,1996
3. Friction Damping of Flutter in Gas Turbine Engine Airfoils;AIAA J. Aircr.,1983
4. Stability of Limit Cycles in Frictionally Damped and Aerodynamically Unstable Rotor Stages;J. Sound Vib.,1985
5. Verification of the Vibration Amplitude Prediction of Self-Excited LPT Rotor Blades Using a Fully Coupled Time-Domain Non-Linear Method and Experimental Data,2008
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