Laminar-turbulent transition in subsonic boundary layers - Research and applications in France
Author:
Affiliation:
1. ONERA, Centre d'Etudes et de Recherches de Toulouse, France
2. ONERA, Chatillon, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1905
Reference33 articles.
1. Analysis of the Instability of the Boundary Layer over a Rotating Disk
2. Viscous interaction phenomena in hypersonic wedge flow
3. Influence of roughness on attachment line boundary layer transition in hypersonic flow
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