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...

Description complète

Enregistré dans:
Détails bibliographiques
Auteurs principaux: Grandhi, Raj Kiran, Roy, Arnab
Format: Article
Langue:anglais
Publié: Research and Development Wing, MIST 2025
Sujets:
Accès en ligne:http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/869
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!