Mixed-Boundary Component Mode Substitution for Nonlinear Dynamics of Mistuned Shrouded Bladed Disks
Author:
Affiliation:
1. Polytechnic University of Turin, 10129 Turin, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades
2. Numerical assessment of friction damping at turbine blade root joints by simultaneous calculation of the static and dynamic contact loads
3. Numerical and Experimental Study of Friction Damping Blade Attachments of Rotating Bladed Disks
4. On Nonlinear Forced Vibration of Shrouded Turbine Blades
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Vibration Characteristics of Mistuned Blisk with Chordwise Variable Thickness Blades Subjected to Aerodynamic Prestress;International Journal of Structural Stability and Dynamics;2023-09-27
2. Numerical Analysis for Optimization of the Lifetime Characteristics of Radial Wheels Turbomachines by Introducing the Intentional Mistuning Parameters;System Analysis & Mathematical Modeling;2023-05-14
3. Relative cyclic component mode synthesis: A reduced order modeling approach for mistuned bladed disks with friction interfaces;Mechanical Systems and Signal Processing;2022-01
4. Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk With Underplatform Dampers;Journal of Engineering for Gas Turbines and Power;2021-02-08
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