Analysis of experimental results of turbomachinery flutter using an asymptotic reduced order model

Author:

Rodríguez Salvador,Martel Carlos

Funder

European Commission

Gobierno de España Ministerio de Ciencia e Innovación

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference23 articles.

1. Flutter-free turbomachinery blades (FUTURE), The European Commission, FP7 project 213414, 2008–2013 (http://www.future-project.eu/).

2. Effect of mistuning and damping on the forced response of a compressor blisk rotor;Beirow,2015

3. Advanced mathematical methods for scientists and engineers: I: Asymptotic methods and perturbation theory;Bender,1999

4. Flutter of mistuned turbomachinery rotors;Bendiksen;J Eng Gas Turb Power,1984

5. Using intentional mistuning in the design of turbomachinery rotors;Castanier;AIAA J,2002

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