The impact of wedge and wavy-wall combustor side walls on shock-induced mixing and combustion in a hydrogen-fuelled model scramjet combustor-Reference-Cited by-同舟云学术

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The impact of wedge and wavy-wall combustor side walls on shock-induced mixing and combustion in a hydrogen-fuelled model scramjet combustor

Published:2024-07 Issue: Volume:74 Page:161-169
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Kummitha Obula Reddy^ORCID

Publisher

Elsevier BV

Reference49 articles.

1. A review of the scramjet experimental database;Seleznev;Prog Aero Sci,2019

2. Supersonic mixing in air breathing propulsion air-breathingsystems for hypersonic flights;Huang;Prog Aero Sci,2019

3. Research progress on mixing enhancement using streamwise vortices in supersonic flows;Hwang;Acta Astronaut,2022

4. Progress toward shock enhancement of supersonic combustion process;Marble,1987

5. On the shock wave enhancement of Confined supersonic mixing flows;Lu;Physics of Fluids A,1991

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