Acoustic Resonance in an Axial Multistage Compressor Leading to Non-Synchronous Blade Vibration
Author:
Affiliation:
1. LMFA, UMR 5509, CNRS, École Centrale de Lyon, Univ. Lyon, F-69134 Ecully, France
2. Safran Helicopter Engines, Safran Group, F-64510 Bordes, France
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/143/9/091014/6696269/turbo_143_9_091014.pdf
Reference21 articles.
1. Non-Engine Order Blade Vibration in a High Pressure Compressor;Baumgartner,1995
2. Blade Excitation by Aerodynamic Instabilities: A Compressor Blade Study;Kielb,2003
3. Acoustic Resonances and Blade Vibration in Axial Flow Compressors;Parker;J. Sound Vib.,1984
4. Acoustic and Convective Mechanisms Contributing to Non-Synchronous-Vibrations in a Multistage Compressor;Brandstetter,2019
5. Non-Synchronous Aeroacoustic Interaction in an Axial Multi-Stage Compressor;Fiquet;ASME J. Turbomach.,2019
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