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