Influence of acoustic reflections on flutter stability of an embedded blade row
Author:
Affiliation:
1. Mechanical Engineering Department, Imperial College London, London, UK
2. Compressor Aeroelasticity, Rolls-Royce Deutschland, Dahlewitz, Germany
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Energy Engineering and Power Technology
Link
http://journals.sagepub.com/doi/pdf/10.1177/0957650915616004
Reference14 articles.
1. INTEGRATION OF 2-D FLUID/STRUCTURE COUPLED SYSTEM FOR CALCULATIONS OF TURBOMACHINERY AERODYNAMIC/ AEROELASTIC INSTABILITIES
2. A Non-Linear Aeroelasticity Analysis of a Fan Blade Using Unstructured Dynamic Meshes
3. Flutter and Resonant Vibration Characteristics of Engine Blades
4. Mechanisms and Prediction Methods for Fan Blade Stall Flutter
5. Prediction of Flutter of Turbine Blades in a Transonic Annular Cascade
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