Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements
Author:
Affiliation:
1. State Key Laboratory of High Temperature Gas Dynamics, Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35689
Reference34 articles.
1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
2. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
3. Numerical Investigation of Combustion/Shock-train Interactions in a Dual-Mode Scramjet Engine
4. Ignition Transient in an Ethylene Fueled Scramjet Engine with Air Throttling Part I: Non-Reacting flow Development and Mixing
5. Ignition Transient in an Ethylene Fueled Scramjet Engine with Air Throttling Part II: Ignition and Flame Development
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