Numerical study on the Re effects on the tip flow structures of transonic fan under inlet distortion-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Numerical study on the Re effects on the tip flow structures of transonic fan under inlet distortion

Published:2023-10 Issue: Volume:141 Page:108530
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Zhiping,Zhu Xingyu^ORCID,Yan Zhaoqi,Pan Tianyu^ORCID,Zheng Xinqian

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Wake ingestion propulsion benefit;Smith;J. Propuls. Power,1993

2. Engine conceptual design studies for a hybrid wing body aircraft;Tong,2009

3. Parametric design studies for propulsive fuselage aircraft concepts;Seitz;CAES Aeronaut. J.,2015

4. Installation effects of a propeller mounted on a high-lift wing with a Coanda flap. Part I: aeroacoustic experiments;Akkermans,2014

5. Installation effects of a propeller mounted on a wing with Coanda flap. Part II: numerical investigation and experimental validation experiments;Dierke,2014

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. Improving large angle flow measurement accuracy of five-hole probe using novel calibration coefficient and accuracy progressive neural network;Flow Measurement and Instrumentation;2024-10

2. Effects of Re on blade load temporal-spatial distribution and correlation with flow stability of transonic compressor under inlet distortion;Aerospace Science and Technology;2024-04

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