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Comparative CFD analysis of a 2D supersonic nozzle flow with jet tab and jet vane

In this study, a CFD (Computational Fluid Dynamics) computational model has been established, with the aim to properly simulate complex supersonic flow generated by a 2D convergent-divergent nozzle. For the purpose of rocket engine thrust vector control (TVC) simulations, initially several jet tab p...

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Detalhes bibliográficos
Main Authors: Olivera Kostić, Zoran Stefanović, Ivan Kostić
Formato: Artigo
Idioma:Inglês
Publicado em: Faculty of Mechanical Engineering in Slavonski Brod, Faculty of Electrical Engineering in Osijek, Faculty of Civil Engineering in Osijek 2017-01-01
Colecção:Tehnički Vjesnik
Assuntos:
Acesso em linha:https://hrcak.srce.hr/file/277442
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