Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp-Reference-Cited by-全球学者库

登录注册会员服务联系我们

Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp

Published:2023-11 Issue: Volume:142 Page:108639
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chen Liang^ORCID,Zhang Yue,Xue Hong-chao^ORCID,Tan Hui-jun,Wang Zi-yun^ORCID,Yu Hang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. How much compression should a scramjet inlet do?;Smart;AIAA J.,2012

2. Busemann inlet for hypersonic speeds;Mölder;J. Spacecr. Rockets,1966

3. Cross section controllable hypersonic inlet design using streamline-tracing and osculating axisymmetric concepts;You,2007

4. Streamline tracing: technique for designing hypersonic vehicles;Billig;J. Propuls. Power,2000

5. Design of modular shape-transition inlets for a conical hypersonic vehicle;Rowan;J. Propuls. Power,2013

全球学者库

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

"全球学者库"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，当前全球学者库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