Ignition characteristics of a high-energy jet plasma igniter in an aeroengine afterburner
Jinlu Yu, Guangxia Chen, Lei Zhang, Zhankai Kang et autres
With the increasing thrust-to-weight ratio demands of modern aeroengines, afterburner ignition performance requirements have become more stringent. To broaden the ignition boundary and enhance ignition capability under extreme conditions, a high-energy jet plasma igniter was developed and its ignition characteristics examined. Analysis …
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Propulsion and Power Research