Prediction of flutter effects on transient flow structure and aeroelasticity of low-pressure turbine cascade using direct numerical simulations
Author:
Funder
Engineering and Physical Sciences Research Council
Publisher
Elsevier BV
Reference44 articles.
1. Design of high accuracy cylindrical profile measurement model for low-pressure turbine shaft of aero engine;Sun;Aerosp. Sci. Technol.,2019
2. Ultra-High Lift Blades for Low Pressure Turbines;Himmel,2010
3. Bladerow interactions, transition, and high-lift aerofoils in low-pressure turbines;Hodson;Annu. Rev. Fluid Mech.,2005
4. Unsteady boundary-layer transition in low-pressure turbines;Coull;J. Fluid Mech.,2011
5. A design method to prevent low pressure turbine blade flutter;Panovsky;J. Eng. Gas Turbines Power,1999
Cited by 14 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. Aeroelastic State of Turbine Rotor During Harmonic Blade Oscillations;Lecture Notes in Mechanical Engineering;2025
2. Location-Based Integration of Internal Lattice Structures in a Turbine Blade for Mass Reduction and Dynamic Characteristic Comparison;International Journal of Aeronautical and Space Sciences;2024-12-15
3. Experimental and numerical study on the impact of inlet temperature inhomogeneity on the aerodynamic performance of a three-stage turbine;Energy;2024-12
4. Impact of internal lattice structures on the weight and natural frequencies of a low pressure turbine blade;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-09-21
5. Hybrid LES/RANS Simulations of Compressible Flow in a Linear Cascade of Flat Blade Profiles;Journal of Thermal Science;2024-07-02
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1.7亿篇,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 © 2019-2025 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