Influence of Intake on Fan Blade Flutter
Author:
Affiliation:
1. Department of Mechanical Engineering, Rolls-Royce Vibration University Technology Centre, Imperial College London, London SW7 2AZ, UK e-mail:
2. Rolls-Royce plc, P.O. Box 31, Derby DE24 8BJ, UK e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4029240/6302945/turbo_137_08_081002.pdf
Reference21 articles.
1. System Mode Shapes in the Flutter of Compressor Blade Rows;J. Aeronaut. Sci.,1956
2. Coupled Blade-Disc-Shroud Flutter Instabilities in Turbojet Engine Rotors;ASME J. Eng. Power,1967
3. A Linearised Unsteady Aerodynamic Analysis for Transonic Cascades;J. Fluid Mech.,1982
4. Recent Advances in the Understanding and Prediction of Turbomachine Subsonic Stall Flutter;ASME J. Eng. Gas Turbines Power,1985
5. Recent Developments in Flutter Suppression Techniques for Turbomachinery Rotors;J. Propul.,1988
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