Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack-Reference-Cited by-同舟云学术

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Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack

Published:2010-02 Issue:2 Volume:22 Page:025105
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Li Xinliang,Fu Dexun,Ma Yanwen

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/1.3313933

Reference19 articles.

1. L. Lees and C. C. Lin, “Investigation of the stability of the laminar boundary layer in compressible fluid,” NACA Report No. TN 1115, 1946.

2. L. M. Mack, “Boundary layer linear stability theory,” AGARD Report No. 709, 1984.

3. K. F. Stetson and R. L. Kimmel, “On hypersonic boundary layer stability,” AIAA Paper No. 92-0737, 1992.

4. K. F. Stetson and R. Kimmel, “On the breakdown of a hypersonic laminar boundary layer,” AIAA Paper No. 93-0896, 1993.

5. A. A. Maslov, S. G. Mironov, and A. A. Shiplyuk, “Hypersonic flow stability experiments,” AIAA Paper No. 2002-0153, 2002.

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