MACH NUMBER INDEPENDENCE OF THE CONICAL SHOCK PRESSURE COEFFICIENT
- 1 October 1963
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (10) , 2389-2391
- https://doi.org/10.2514/3.2074
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- The Combined Supersonic-Hypersonic Similarity RuleJournal of the Aeronautical Sciences, 1951
- A Note on the Calculation of Oblique Shock-Wave CharacteristicsJournal of the Aeronautical Sciences, 1950