Laminar boundary layer with constant wall shear stress.
- 1 December 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (12) , 2432-2434
- https://doi.org/10.2514/3.5011
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Triple-Shock-Wave IntersectionsPhysics of Fluids, 1959
- On fully-dispersed shock waves in carbon dioxideJournal of Fluid Mechanics, 1957