Compressible Turbulent Boundary Layer on a Yawed Cone
Author:
Affiliation:
1. Institut de Mecanique des Fluides, Marseille, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61396
Reference7 articles.
1. Three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic flow
2. 3Michel, R., Quemard, C., and Cousteix, J. "Application d'un Schema Ameliore de Longueur de Melange a Letude des Couches Limites Turbulentes Tridimensionnelles," AGARD-CP No. 93, Ref. 7,1971.
3. NUMERICAL SOLUTION OF THE TURBULENT-BOUNDARY-LAYER EQUATIONS
4. Supersonic Turbulent Boundary Layer in the Symmetry Plane of a Gone at Incidence
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