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...

Volledige beschrijving

Bewaard in:
Bibliografische gegevens
Hoofdauteurs: Grandhi, Raj Kiran, Roy, Arnab
Formaat: Artikel
Taal:Engels
Gepubliceerd in: Research and Development Wing, MIST 2025
Onderwerpen:
Online toegang:http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/869
Tags: Voeg label toe
Geen labels, Wees de eerste die dit record labelt!