Blade thickness effects on viscous flutter in a radial turbocharger turbine-Reference-Cited by-同舟云学术

Blade thickness effects on viscous flutter in a radial turbocharger turbine

Published:2022-06 Issue: Volume:136 Page:106139
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Sajedin Azadeh,Allport John,Amoozgar Mohammadreza,Marandi Omid Farhangiyan

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference24 articles.

1. D. Vogt, Experimental investigation of three-dimensional mechanisms in low-pressure turbine flutter. PhD Thesis, Royal Institute of Technology, Department of Heat and Power Technology, Stockholm, Sweden, 2005.

2. A review of aeroelasticity methods with emphasis on turbomachinery applications;Marshall;J. Fluids Struct.,1996

3. Flutter and resonant vibration characteristics of engine blades;Srinivasan;ASME J. Eng. Gas Turbines Power,1997

4. Coupled bending-torsion flutter in a supersonic cascade;Bendiksen,1980

5. A parametric study of the flutter stability of two-dimensional turbine and compressor cascades in incompressible flow;Forsching;Zeitschrift fur Flugwissenschaften and Weltraumforschung,1989

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