Computational Investigation of Effects of Side-Injection Geometry on Thrust-Vectoring Performance in a Fuel-Injected Dual Throat Nozzle

Dual-throat Nozzle (DTN) is known as one of the most effective approaches of fluidic thrust-vectoring. It is gradually flourishing into a promising technology to implement supersonic and hypersonic thrust-vector control in aircrafts. The main objective of the present study is numerical investigation...

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Bibliographic Details
Main Authors: M. R. Salimi, R. Askari, M. Hasani
Format: Article
Language:English
Published: Isfahan University of Technology 2022-05-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:https://www.jafmonline.net/article_2055_18e18538d6dd9156c1a140a8848bfa2e.pdf