Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method-Reference-Cited by-同舟云学术

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Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Kashitani Masashi¹,Yamaguchi Yutaka¹,Kitano Hideki¹

Affiliation:

1. National Defense Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-983

Reference12 articles.

1. 1G.S.Settles,SchlierenandShadowgraphTechnique,Springer,(2001).

2. Measurements in a subsonic turbulent jet using a quantitative schlieren technique

3. 4L.M.Weinstein,AnImprovedLarge-FieldFocusingSchlierenSystem,AIAApaper91-0567,(1991).

4. 5E.Gartengerg,L.M.Weinstein,andE.E.LeeJr.,Aerodynamic Investigation withFocusingSchlieren inaCryogenicWind Tunnel,AIAA J.,32,(1994),pp.1242-1249.

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. Basic Experiment on Focusing Schlieren PIV Method with LED Light Source;31st International Symposium on Shock Waves 1;2019

2. Fundamental Study on Operational Parameters of Diaphragmless Shock Tube;MATEC Web of Conferences;2018

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