On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating
Author:
Affiliation:
1. ONERA/DMAS, F-59014 Lille, France
2. Univ. Lille, CNRS, Centrale Lille, UMR 9013 - LaMcube - Laboratoire de Mécanique, Multiphysique, Multi-échelle, F-59000 Lille, France
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/144/5/051008/6821909/turbo_144_5_051008.pdf
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2. Flutter and Resonant Vibration Characteristics of Engine Blades;Srinivasan;ASME J. Eng. Gas Turbines Power,1997
3. Dynamic Modeling and Vibration Characteristics Analysis of the Aero-Engine Dual-Rotor System With Fan Blade Out;Yu;Mech. Syst. Signal. Process.,2018
4. Common Failures in Gas Turbine Blades;Carter;Eng. Failure Anal.,2005
5. Failure Analysis of a Set of Compressor Blades;Silveira;Eng. Failure Anal.,2008
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