Flow Visualization Measurement Techniques for High-Speed Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel

Author:

Matsumura Shin1,Schneider Steven1,Berry Scott2

Affiliation:

1. Purdue University

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Cited by 9 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. Heat-Flux Measurements with Temperature-Sensitive Paint in a Mach-6 Quiet Tunnel;Journal of Spacecraft and Rockets;2013-03

2. Correcting lateral heat conduction effect in image-based heat flux measurements as an inverse problem;International Journal of Heat and Mass Transfer;2011-02

3. Numerical Inverse Heat Transfer Analysis for Temperature-Sensitive-Paint Measurements in Hypersonic Tunnels;Journal of Thermophysics and Heat Transfer;2011-01

4. Analytical Method for Determining Heat Flux from Temperature-Sensitive-Paint Measurements in Hypersonic Tunnels;Journal of Thermophysics and Heat Transfer;2010-01

5. Effect of Freestream Noise on Instability and Transition for the X-51A Lee Side;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

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

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3