Tip Clearance Effects on Aero-elastic Stability of Axial Compressor Blades
Author:
Affiliation:
1. School of Energy and Power Engineering, Beihang University, 37 Xueyuan Road, Haidian District, Beijing 100191, China 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/10.1115/1.4028019/6162817/gtp_137_01_012501.pdf
Reference22 articles.
1. Flutter Prediction of a Transonic Fan With Travelling Wave Using Fully Coupled Fluid/Structure Interaction,2013
2. Flutter Prediction in Turbomachinery With Energy Method;Proc. Inst. Mech. Eng., Part G,2011
3. Flutter Mechanisms in Low Pressure Turbine Blades;ASME J. Eng. Gas. Turbines Power,2000
4. Mechanisms and Prediction Methods for Fan Blade Stall Flutter;J. Propul. Power,2001
5. Mechanisms and Key Parameters for Compressor Blade Stall Flutter;ASME J. Turbomach.,2013
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