Non-reacting flow visualization of supersonic combustor based on cavity and cavity–strut flameholder
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference22 articles.
1. Review of cavity-stabilized combustion for scramjet applications;Wang;Proc. Inst. Mech. Eng. Part G—J. Aerosp. Eng.,2014
2. Fundamental studies of cavity-based flameholder concepts for supersonic combustors;Gruber;J. Propuls. Power,2001
3. Cavity flame-holders for ignition and flame stabilization in scramjets: an overview;Ben-Yakar;J. Propuls. Power,2001
4. Large eddy simulation based studies of jet-cavity interactions in a supersonic flow;Wang;Acta Astronaut.,2014
5. Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity;Wang;Acta Astronaut.,2015
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