Detached Eddy Simulations of a Reaction Control Jet from an Axi-Symmetric Body in a Supersonic Crossflow
The introduction of a control jet into a supersonic cross flow yields a substantial region of separated flow, manifesting in the vicinity of the injection site. This, in turn, alters the distribution of pressure on the primary body, thereby influencing the effectiveness of the injected jet’s capa...
में बचाया:
| मुख्य लेखकों: | , |
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| स्वरूप: | लेख |
| भाषा: | अंग्रेज़ी |
| प्रकाशित: |
Research and Development Wing, MIST
2025
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| विषय: | |
| ऑनलाइन पहुंच: | http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/869 |
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