Design of mistuning patterns to control the vibration amplitude of unstable rotor blades
Author:
Funder
European Commission
Industria de Turbopropulsores S.A.U.
Ministerio de Economía y Competitividad
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference30 articles.
1. Modeling and analysis of mistuned bladed disk status and emerging directions;Castanier;J. Propuls. Power,2006
2. Flutter and response of a mistuned cascade in incompressible flow;Kaza;AIAA J.,1982
3. Effects of structural coupling on mistuned cascade flutter and response;Kielb;J. Eng. Gas Turbines Power,1984
4. Optimization and mechanisms of mistuning in cascades;Crawley;J. Eng. Gas Turbines Power,1985
5. Aerodynamic and structural detuning of supersonic turbomachine rotors;Hoyniak;J. Propuls. Power,1986
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