Effect of Radical Addition on Extinction Limits of H2 and CH4 Flames
Author:
Affiliation:
1. Tohoku University
2. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1029
Reference22 articles.
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2. 2Northam,G.B., McClinton,C.R., Wagner,T.C., and O'Brien,W.F. "Development and Evaluation of a Plasma Jet Flameholder for Scramjets,"AIAAPaper84-1408, June 1984.
3. Scramjet Engine Tests at Mach 4 and 6
4. Some governing parameters of plasma torch igniter/flameholder in a scramjet combustor
5. Effects of Airstream Mach Number on H/N Plasma Igniter
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