Stagnation Point of a Blunt Body in Hypersonic Flow
- 1 January 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (1), 25-32
- https://doi.org/10.2514/8.3759
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- On an Integral Equation in the Supersonic Oscillating Wing TheoryJournal of the Aeronautical Sciences, 1953