Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20

Published:1971-05 Issue:5 Volume:9 Page:826-834
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

FISCHER M. C.¹,MADDALON D. V.¹,WEINSTEIN L. M.¹,WAGNER R. D.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.6282

Reference30 articles.

Cited by 33 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. Free-stream static pressure measurements in the Longshot hypersonic wind tunnel and sensitivity analysis;Experiments in Fluids;2016-04-16

2. Design of Static Pressure Probes for Improved Free-Stream Characterization in Hypersonic Wind-Tunnels;52nd Aerospace Sciences Meeting;2014-01-10

3. Pressure fluctuations within a turbulent gas flow and their interaction with a shock wave;Moscow University Physics Bulletin;2013-03

4. Wave processes in a viscous shock layer and control of fluctuations;Journal of Fluid Mechanics;2010-03-18

5. Experimental study and direct numerical simulation of the evolution of disturbances in a viscous shock layer on a flat plate;Journal of Applied Mechanics and Technical Physics;2006-09

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