Hypersonic laminar boundary layer approaching the base of a slender body.
- 1 July 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (7) , 1261-1267
- https://doi.org/10.2514/3.5332
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Upstream influence of the base pressure.AIAA Journal, 1968
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Transonic rotational flow over a convex cornerJournal of Fluid Mechanics, 1960
- Elements of GasdynamicsPhysics Today, 1957
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953