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Tag Archives: Wide Range Aeroengine

Preliminary Study of High-speed Variable Geometry Two-dimensional Inlet Design

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 13, 2024

Jun LIU, Xueju QIU, Huacheng YUAN

DOI Number: 10.60853/7x0z-1×39

Conference number: HiSST-2024-0095

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