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Ignition characteristics of a high-energy jet plasma igniter in an aeroengine afterburner

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 igniti...

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Bibliografiske detaljer
Principais autores: Jinlu Yu, Guangxia Chen, Lei Zhang, Zhankai Kang, Luyun Jiang, Yang Yu, Xiangyu Zhu, Gaofeng Wang
Format: Artigo
Sprog:Inglês
Udgivet: KeAi Communications Co., Ltd. 2026-06-01
Serier:Propulsion and Power Research
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Online adgang:http://www.sciencedirect.com/science/article/pii/S2212540X26000404
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