Influence of Contraction Section Shape and Inlet Flow Direction on Supersonic Nozzle Flow and Performance
- 1 June 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (6) , 420-427
- https://doi.org/10.2514/3.61705
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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