Non-synchronous blade vibration analysis of a transonic fan
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference36 articles.
1. Aeroelastic simulation of the first 1.5-stage aeroengine fan at rotating stall;Liang;Chin J Aeronaut,2020
2. Aeroelastic analysis and structural parametric design of composite rotor blade;Ma;Chin J Aeronaut,2021
3. Aeroelastic prediction and analysis for a transonic fan rotor with the “hot” blade shape;Zhou;Chin J Aeronaut,2021
4. Role of tip clearance flow in rotating instabilities and nonsynchronous vibrations;Vo;J Propuls Power,2010
5. Blade tip clearance flow and compressor nonsynchronous vibrations: The jet core feedback theory as the coupling mechanism;Thomassin;J Turbomach,2009
Cited by 9 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. Blade aerodynamic force and tip region vortex spatial-temporal evolution study of a compressor cascade;Aerospace Science and Technology;2024-02
2. Numerical Investigation of Classic Flutter Mechanism Under Circumferentially Non-Uniform Inlet Condition;Journal of Turbomachinery;2024-01-29
3. Experimental and Numerical Investigation of Non-synchronous Blade Vibration Excitation in a Transonic Axial Compressor;Journal of Thermal Science;2024-01-24
4. Flutter analysis of compressor blades under travelling wave modes using an efficient fluid–structure interaction method;Chinese Journal of Aeronautics;2023-11
5. Analysis of Tip Leakage Vortex Instability and Blade Force in a Low-Speed Compressor Cascade;2023-09-01
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