Simulations of combustion with normal and angled hydrogen injection in a cavity-based supersonic combustor
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, China
2. Department of Mechanical Engineering, University of Sheffield, Sheffield, UK
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410013475567
Reference34 articles.
1. Supersonic Combustion Experiments with a Cavity-Based Fuel Injector
2. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
3. Supersonic combustion of cross-flow jets and the influence of cavity flame-holders
4. Reaction Zone Imaging in a Dual-Mode Scramjet Combustor Using CH-PLIF
5. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder
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