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Investigation on the Aerodynamic Performance and Flow Mechanism of Transonic Ultra-Highly Loaded Tandem-Rotor Stage

The compressor serves as a crucial component that influences the performance of the gas turbine engine. Researchers have been endeavoring to explore compressor types that possess a high loading level and high-efficiency characteristics concurrently. In this study, tandem blade technology was applied...

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Hlavní autoři: Shilong Yuan, Yunfeng Wu, Shengfeng Zhao, Xingen Lu, Ge Han
Médium: Artigo
Jazyk:Inglês
Vydáno: MDPI AG 2024-05-01
Edice:Aerospace
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On-line přístup:https://www.mdpi.com/2226-4310/11/5/389
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