Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible Flow
- 1 October 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (10) , 671-675
- https://doi.org/10.2514/8.2076
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The laminar boundary layer in compressible flowPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1948