Three-Dimensional Numerical Simulation of Görtler Vortices in Hypersonic Compression Ramp-Reference-Cited by-同舟云学术

Three-Dimensional Numerical Simulation of Görtler Vortices in Hypersonic Compression Ramp

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Ohmichi Yuya¹,Suzuki Kojiro¹

Affiliation:

1. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-262

Reference15 articles.

1. 1Görtler,H."Onthethree-dimensionalinstabilityoflaminarboundarylayersonconcavewalls,"NACATM-1375,1954.

2. 2Liepman, H. W. "Investigation of laminar boundary layer stability and transition on curved boundaries," NACA Wartime Report, ACR 3H30,1943.

3. 4Kashiwa Wind Tunnel Working Group. "UT-Kashiwa Hypersonic and High-Temperature Wind Tunnel," URL:http://daedalus.k.u-tokyo.ac.jp/wt/wt_index.htm[cited20Dec2012].

4. 5Morita,K.,Suzuki,K.,Imamura,O.andSakaue,H."Temperature-CancelledAnodized-AluminumPressureSensitivePaint for HypersonicWind Tunnel Application,"AIAA Paper,2011-3724.

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