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Numerical assessment of friction damping at turbine blade root joints by simultaneous calculation of the static and dynamic contact loads
Authors:Stefano Zucca  Christian M Firrone  Muzio M Gola
Institution:(1) Department of Mechanical Engineering, Politecnico di Torino, Corso Duca degli Abruzzi, 24, Torino, Italy
Abstract:In turbomachinery, the perfect detuning of turbine blades in order to avoid high cycle fatigue damage due to resonant vibration is often unfeasible due to the high modal density of bladed disks.
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