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Experimental study on dielectric barrier discharge plasma-assisted combustion for nozzle
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Journal Article
Experimental study on dielectric barrier discharge plasma-assisted combustion for nozzle
2019
Overview
Aiming at the structure of small thrust rocket engine injector, a coaxial shear-type dielectric barrier discharge plasma nozzle was designed, and the effects of methane discharge and air discharge on combustion effect under different excitation and different mixing ratio conditions are studied. The results show that: the flashback occurs when the methane discharge voltage is high, the air discharge can broaden the blow off limit of the air/methane diffusion flame, and has the effect of stabilizing the flame and reducing the lift height.
Publisher
IOP Publishing
Subject
