Two-Dimensional and Axisymmetric Rotational Flows Past a Transonic Corner
- 1 April 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (4) , 503-504
- https://doi.org/10.2514/8.9533
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Direct Calculation of Pressure Distribution on Blunt Hypersonic Nose Shapes With Sharp CornersJournal of the Aerospace Sciences, 1961
- Transonic rotational flow over a convex cornerJournal of Fluid Mechanics, 1960
- On the Flow Behind Curved ShocksJournal of Mathematics and Physics, 1948