A Note on the Laminar Boundary Layer on a Circular Cylinder in Axial Incompressible Flow
Author:
Affiliation:
1. U.S. Naval Ordnance Test Station, Inyokern, China Lake, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3151
Reference2 articles.
1. Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible Flow
2. Simplified Treatment of the Turbulent Boundary Layer Along a Cylinder in Compressible Flow
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