Direct numerical simulation of breakdown to turbulence in a Mach 6 boundary layer over a porous surface-Reference-Cited by-同舟云学术

Direct numerical simulation of breakdown to turbulence in a Mach 6 boundary layer over a porous surface

Published:2010-09 Issue:9 Volume:22 Page:094105
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

De Tullio Nicola,Sandham Neil D.

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/10.1063/1.3481147

Reference46 articles.

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

2. L. M. Mack, “Boundary layer linear stability theory,” AGARD Technical Report No. 705, 1984.

3. L. Lees, “The stability of the laminar boundary layer in a compressible fluid,” NACA Technical Report No. 1360, 1947.

4. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition

5. The effect of cooling on supersonic boundary-layer stability

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