Robust design of turbine blades with friction contacts in the presence of multiple response levels

Author:

Zara GianmarcoORCID,Ferhatoglu Erhan,Berruti Teresa Maria,Zucca Stefano

Publisher

Elsevier BV

Reference34 articles.

1. High cycle fatigue in aircraft gas turbines—an industry perspective;Cowles;Int. J. Fract.,1996

2. Underplatform dampers for turbine blades: theoretical modeling, analysis, and comparison with experimental data;Sanliturk;J. Eng. Gas Turbines Power,2001

3. Forced response prediction of constrained and unconstrained structures coupled through frictional contacts;Cigeroglu;J. Eng. Gas Turbines Power,2009

4. Modelling the nonlinear behaviour of an underplatform damper test rig for turbine applications;Pesaresi;Mech. Syst. Signal Process.,2017

5. Forced response analysis of integrally bladed disks with friction ring dampers;Laxalde;J. Vib. Acoust. Trans. ASME,2010

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