Experimental and Computational Study of a Tuned Damper with Frictional Contacts
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference20 articles.
1. Bolt Modeling Effects on Fatigue Predictions for Mock Hardware in a Random Vibration Environment
2. Influence of Geometric Design Parameters Onto Vibratory Response and High-Cycle Fatigue Safety for Turbine Blades With Friction Damper
3. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
4. Qualitative analysis of forced response of blisks with friction ring dampers
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1. Experimental and Numerical Investigation of Dynamic Vibration Absorber Array for Vibration Mitigation of Integral Blisk;Journal of Engineering for Gas Turbines and Power;2024-08-21
2. Intentional Blade Mistuning to Emulate the Dynamic Influence of Split Ring Damper;Journal of Vibration and Acoustics;2024-04-01
3. Resonant Vibration Absorbers with Impacts;Nonlinear Structures & Systems, Volume 1;2023-10-14
4. The Vibration Attenuation Characteristics of Dynamic Vibration Absorbers Array for Tuned and Mistuned Bladed Disk;Journal of Engineering for Gas Turbines and Power;2023-09-07
5. Particle swarm optimization of friction tuned mass dampers subjected to ground motion records;Soil Dynamics and Earthquake Engineering;2023-09
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