Hypersonic Flow Near the Forward Stagnation Point of a Blunt Body of Revolution
- 1 December 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (12) , 789-790
- https://doi.org/10.2514/8.7891
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Magneto-Hydrodynamic ShocksPhysical Review B, 1950