Asymptotic description of damping mistuning effects on the forced response of turbomachinery bladed disks

Author:

Khemiri O.,Martel C.,Corral R.

Funder

Spanish Ministerio de Educación y Ciencia

Universidad Politécnica de Madrid

EOARD

Publisher

Elsevier BV

Subject

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

Reference16 articles.

1. Forced response of bladed disk assemblies—a survey;Slater;The Shock and Vibration Digest,1999

2. Modeling and analysis of mistuned bladed disk status and emerging directions;Castanier;Journal of Propulsion and Power,2006

3. D. Ewins, The mistuned blade vibration problem re-visited, Twelfth International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, 2009, p. 323.

4. D. Hemberger, D. Filsinger, H.-J. Bauer, Investigations on maximum amplitude amplification factor of real mistuned bladed structures, Presented at the ASME Turbo Expo, Copenhauen, Denmark, 2012, ASME Paper GT2012-68084.

5. Effects of damping and damping mistuning on the forced response vibrations of bladed disks;Lin;Journal of Sound and Vibration,1996

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