Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion

Published:2012-09-24 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Chan Wilson Y. K.¹,Mee David¹,Smart Michael¹,Turner James¹

Affiliation:

1. University of Queensland

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5889

Reference43 articles.

1. Hypervelocity Skin-Friction Reduction by Boundary-Layer Combustion of Hydrogen

2. 2Denman, A. W., Large-eddy simulation of compressible turbulent boundary layers with heat addition, PhD thesis,The University of Queensland, Queensland, Australia, 2007.

3. Shock-Tunnel Skin-Friction Measurement

4. Skin-Friction Measurements in a Supersonic Combustor with Crossflow Fuel Injection

5. 5Kirchhartz, R. M., Upstream wall layer effects on drag reduction with boundary layer combustion, PhD thesis,The University of Queensland, Queensland, Australia, 2010.

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. The T4 Stalker Tube;30th International Symposium on Shock Waves 2;2017

2. Free Piston Shock Tunnels HEG, HIEST, T4 and T5;Experimental Methods of Shock Wave Research;2015-11-01

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