Shock-Capturing, Finite-Difference Approach to Supersonic Flows
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (12) , 1175-1182
- https://doi.org/10.2514/3.59785
Abstract
No abstract availableKeywords
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