Instationäre grenzschichten hinter verdichtungsstössen und expansionswellen-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Instationäre grenzschichten hinter verdichtungsstössen und expansionswellen

Published:1961-01 Issue: Volume:1 Page:104-173
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:de
Short-container-title:Progress in Aerospace Sciences

Author:

Becker von E.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference85 articles.

1. Das Anwachsen der Grenzschicht in und hinter einer Expansionswelle;Becker;Ing. Arch.,1957

2. Die laminare, kompressible Grenzschicht in einer Expansionswelle;Becker,1957

3. Reibungswirkungen beim Rohrwindkanal;Becker,1958

4. On the laminar boundary layer generated by a travelling shock;Bershader;Bull. Am. Phys. Soc.,1956

Cited by 13 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

2. Transition boundary between regular and Mach reflections for a moving shock interacting with a wedge in inviscid and polytropic argon;Shock Waves;2019-01-07

3. Experimental characterization of the transonic test section flow in a Ludwieg tube;Aerospace Science and Technology;2018-10

4. Inlet Measurements and Quiet Flow Improvements in the Boeing/AFOSR Mach-6 Quiet Tunnel;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

5. Effect of boundary layer on Mach reflection over a wedge surface;Shock Waves;2002-01-01

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