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...

Täydet tiedot

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Bibliografiset tiedot
Päätekijät: Grandhi, Raj Kiran, Roy, Arnab
Aineistotyyppi: Artikkeli
Kieli:englanti
Julkaistu: Research and Development Wing, MIST 2025
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Linkit:http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/869
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