Abstract The calculation made on the basis of simple mathematical models are presented for evaluating the temperature and thermal capacity of a plasma plug flame in the GTE afterburner in a wide range of startup conditions.
Application of a plasma ignition system to ignite kerosene-air mixture in the GTE afterburner in a wide range of its startup conditions
Russian Aeronautics (Iz VUZ) ; 53 , 3 ; 349-352
2010-09-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
Online Contents | 2013
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