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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| Auteurs principaux: | , , , , , , , |
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| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
KeAi Communications Co., Ltd.
2026-06-01
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| Collection: | Propulsion and Power Research |
| Sujets: | |
| Accès en ligne: | http://www.sciencedirect.com/science/article/pii/S2212540X26000404 |
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