Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity-Reference-Cited by-同舟云学术

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Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity

Published:2021-11 Issue: Volume:188 Page:491-504
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Anyoji Masayuki^ORCID,Akagi Fujio^ORCID,Matsuda Yu^ORCID,Egami Yasuhiro^ORCID,Handa Taro^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Hypersonic Airbreathing Propulsion. AIAA Education Series;Heiser,1994

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

3. A review of the scramjet experimental data base;Seleznev;Prog. Aero. Sci.,2019

4. Experimental supersonic combustion research at NASA Langley;Rogers;AIAA Pap,1998

5. Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity;Gerlinger;Aero. Sci. Technol.,2008

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1. Investigation of multi-scale flow structures and combustion characteristics in a cavity-enhanced circular scramjet;Combustion and Flame;2024-06

2. Improving the combustion of scramjet engines with struts using grooves and bumps;Aerospace Science and Technology;2024-04

3. Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector mode;Aerospace Science and Technology;2023-07

4. On aerodynamic characteristics of rarefied hypersonic flows over variable eccentricity elliptical cavities;Aerospace Science and Technology;2023-03

5. Influence of Incident Shocks on Flame Characteristics in the Strut-Equipped Supersonic Combustor;AIAA Journal;2023-01

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