Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor-Reference-Cited by-同舟云学术

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Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor

Published:2021-11 Issue: Volume:188 Page:426-437
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Choubey Gautam^ORCID,Yadav Pabbala Monish^ORCID,Devarajan Yuvarajan,Huang Wei^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference93 articles.

1. A review on hydrogen industrial aerospace applications;Cecere;Int. J. Hydrogen Energy,2014

2. Research on supersonic combustion;Billig;J. Propul. Power,1993

3. Scramjet engines: the first forty years;Curran;J. Propul. Power,2001

4. Numerical studies on the performance of scramjet combustor with alternating wedge-shaped strut injector;Choubey;Int. J. Turbo Jet Eng.,2017

5. Numerical study on turbulent structure of transverse jet into a supersonic flow;Watanabe,2011

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