A Note on the Laminar Boundary Layer on a Circular Cylinder in Axial Incompressible Flow
- 1 September 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (9), 634
- https://doi.org/10.2514/8.3151
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Simplified Treatment of the Turbulent Boundary Layer Along a Cylinder in Compressible FlowJournal of the Aeronautical Sciences, 1952
- Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible FlowJournal of the Aeronautical Sciences, 1951