Investigation of flow separation over a rearward-facing step in a hypersonic stream.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 986-987
- https://doi.org/10.2514/3.4663
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- On the separation of a supersonic flow at a sharp corner.AIAA Journal, 1967
- Effect of a shoulder modification on turbulent supersonic base flow.AIAA Journal, 1967
- An experimental study of supersonic flow over a rearward facing step.AIAA Journal, 1967
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- The base-flow and near-wake problem at very low Reynolds numbers Part 2. The Oseen approximationJournal of Fluid Mechanics, 1965
- The base-flow and near-wake problem at very low Reynolds numbers - Part 1. The Stokes approximationJournal of Fluid Mechanics, 1965