Experimental and numerical investigation of periodic downstream potential flow on the behavior of boundary layer of high-lift low-pressure turbine blade-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Experimental and numerical investigation of periodic downstream potential flow on the behavior of boundary layer of high-lift low-pressure turbine blade

Published:2022-04 Issue: Volume:123 Page:107453
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Shuang,Wu Xingshuang,Huang Zhen,Hu Xizhuo,Zhang Peng,Kong Qingguo

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. The role of transition in high-lift low-pressure turbines for aeroengines;Hodson;Prog. Aerosp. Sci.,2005

2. Designing low pressure turbines for optimized airfoil lift;Gier;J. Turbomach.,2010

3. Boundary layer development in the BR710 and BR715 LP turbines: the implementation of high lift and ultra high lift concepts;Howell;J. Turbomach.,2002

4. Aerodynamic Design of Low Pressure Turbines;Hourmouziadis,1989

5. The role of laminar-turbulent transition in gas turbine engines;Mayle;J. Eng. Gas Turbines Power,1991

Cited by 2 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. Analysis of the Effect of the Leading-Edge Vortex Structure on Unsteady Secondary Flow at the Endwall of a High-Lift Low-Pressure Turbine;Aerospace;2023-02-28

2. Computer Flow Simulation and Verification for Turbine Blade Channel Formed by the C-90-22 A Profile;Inventions;2022-08-04

同舟云学术

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