Numerical assessment of friction damping at turbine blade root joints by simultaneous calculation of the static and dynamic contact loads

被引:0
作者
Stefano Zucca
Christian M. Firrone
Muzio M. Gola
机构
[1] Politecnico di Torino,Mech. Eng. Dept.
来源
Nonlinear Dynamics | 2012年 / 67卷
关键词
Turbine blade; Blade root; Friction damping; Forced response; Harmonic balance;
D O I
暂无
中图分类号
学科分类号
摘要
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.
引用
收藏
页码:1943 / 1955
页数:12
相关论文
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