Transpiration cooling in a laminar boundary layer with solid wall upstream effects.
- 1 February 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (2) , 193-197
- https://doi.org/10.2514/3.4477
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Nonsimilar Solutions of the Compressible-Laminar Boundary-Layer Equations With Applications to the Upstream-Transpiration Cooling ProblemJournal of the Aerospace Sciences, 1961
- On the solution of the laminar boundary layer equations.Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1938
- Note on the velocity distribution in the wake behind a flat plate placed along the streamMathematical Proceedings of the Cambridge Philosophical Society, 1936