Combustion stabilization modes in a hydrogen-fueled scramjet combustor at high stagnation temperature
Authors:
- 1 November 2018
- journal article
- research article
- Published by Elsevier in Acta Astronautica
- Vol. 152, 112-122
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51406232, 11472305)
This publication has 27 references indexed in Scilit:
- Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustorInternational Journal of Hydrogen Energy, 2013
- Experimental study of oscillations in a scramjet combustor with cavity flameholdersExperimental Thermal and Fluid Science, 2013
- Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholderProceedings of the Combustion Institute, 2013
- Combustion characteristics of a dual-mode scramjet combustor with cavity flameholderProceedings of the Combustion Institute, 2009
- Flame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity FlameholderJournal of Propulsion and Power, 2008
- X-43A Hypersonic vehicle technology developmentActa Astronautica, 2006
- Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic FlowJournal of Propulsion and Power, 2004
- Supersonic Combustion Experiments with a Cavity-Based Fuel InjectorJournal of Propulsion and Power, 2001
- Scramjet Engines: The First Forty YearsJournal of Propulsion and Power, 2001
- Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An OverviewJournal of Propulsion and Power, 2001