Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2125
2. McGill University, Montreal, Quebec H3A 2K6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13172
Reference32 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades
2. Forced Response of Bladed Disk Assemblies--A Survey
3. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
4. Coupling of Turbomachine Blade Vibrations Through the Rotor
5. Vibration Amplitudes of Compressor Blades Resulting From Scatter in Blade Natural Frequencies
Cited by 161 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. Reduced order modeling and mistuning identification method for rotating bladed disks under varying speeds;Journal of Sound and Vibration;2025-01
2. Influence of Regeneration-Induced Mistuning on the Aeroelasticity of Multistage Axial Compressors;Regeneration of Complex Capital Goods;2024-09-12
3. An Optimization Method for Stiffness and Damping Mistuning Identification From Blade Tip Timing Data;Journal of Engineering for Gas Turbines and Power;2024-08-23
4. 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
5. Nonlinear dynamic prediction and design optimization of bladed-disk based on hybrid deep neural network;International Journal of Non-Linear Mechanics;2024-06
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3