Experimental study of ignition and combustion characteristics of ethylene in cavity-based supersonic combustor at low stagnation temperature and pressure
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference50 articles.
1. Hypersonic propulsion
2. Recent advances in cavity-based scramjet engine- a brief review
3. Effect of fuel-jet injection angle variation on the overall performance of a SCRAMJET engine
4. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
5. Investigation of combustion process of a kerosene fueled combustor with air throttling
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