Three dimensional CFD investigation of shock train structure in a supersonic nozzle-Reference-Cited by-同舟云学术

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Three dimensional CFD investigation of shock train structure in a supersonic nozzle

Published:2015-11 Issue: Volume:116 Page:56-67
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kamali Reza^ORCID,Mousavi Seyed Mahmood,Binesh Ali Reza

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Classification of pseudo-steady shock wave reflection types;Semenov;Shock Waves,2012

2. Behavior of shock trains in a diverging duct;Weiss;Exp. Fluids,2010

3. Isolator/combustion chamber interactions during supersonic combustion;Tu;J. Propuls. Power,2010

4. Behaviour of a shock train under the influence of boundary-layer suction by a normal slot;Weiss;Exp. Fluids,2012

5. Flow field characteristics of a transverse jet into supersonic flow with pseudo-shock wave;Yamauchi;Shock Waves,2012

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