Investigation of turbulence flow characteristics in a dual-mode scramjet combustor using hydroxyl tagging velocimetry
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference26 articles.
1. Nonlinear Characteristics and detection of combustion Modes for a Hydrocarbon fueled scramjet;Zhang;Acta Astronaut.,2015
2. Shock wave structures in the wake of sonic transverse jet into a supersonic crossflow;Liang;Acta Astronaut.,2018
3. Turbulence/chemistry interactions in a ramp-stabilized supersonic hydrogen–air diffusion flame;Fulton;Combust. Flame,2016
4. Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor;Zhang;Acta Astronaut.,2017
5. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder;Micka;Proc. Combust. Inst.,2009
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