Unsteady Flow Measurements in a Front Loaded Low Pressure Turbine Passage
Author:
Affiliation:
1. Air Force Research Laboratory
2. Wright State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2124
Reference16 articles.
1. McQuilling, M. W. "Design and Validation of a High-Lift Low-Pressure Turbine Blade," Ph.D. Dissertation,Wright State University, 2007.
2. Determination of mean and dynamic skin friction, separation and transition in low-speed flow with a thin-film heated element
3. Boundary Layer and Loss Measurements on the Rotor of an Axial-Flow Turbine
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. Vortex Unsteadiness in the Endwall Region of a High-Lift Low-Pressure Turbine Passage;Journal of Turbomachinery;2022-10-07
2. Numerical Investigation of Effect of Stator and Bar Wake Generator on Low-Pressure Turbine Endwall Flow;AIAA SCITECH 2022 Forum;2022-01-03
3. Numerical Investigation of Turbulent Junction Flows;AIAA Journal;2021-11
4. Numerical Investigation of 50% Reaction Low-PressureTurbine Stage;AIAA AVIATION 2021 FORUM;2021-07-28
5. Numerical Investigation of Turbulent Junction Flow Horseshoe Vortex Dynamics;AIAA Journal;2021-04
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