The Effect of Slip, Particularly for Highly Cooled Walls
- 1 May 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (5) , 591-595
- https://doi.org/10.2514/8.9563
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- First-Order Slip Effects on the Compressible Laminar Boundary Layer Over a Slender Body of Revolution in Axial FlowJournal of the Aerospace Sciences, 1961
- Vorticity Effect on the Stagnation-Point Flow of a Viscous Incompressible FluidJournal of the Aerospace Sciences, 1959