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Numerical Investigations and Optimized Design of the Active Cooling Performance with Phase Change for Aircraft Rudder Shaft

During hypersonic flight, the air rudder shaft can undergo huge aerodynamic heating load, where it is necessary to design the thermal protection system of the air rudder shaft. Aiming to prevent the rudder shaft from thermal failure due to the heat endurance limit of materials, numerical investigati...

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Principais autores: Xiangchun Sun, Kaiyan Jin, Kuan Zhao, Hexuan Zhang, Guice Yao, Dongsheng Wen
Formato: Artigo
Idioma:Inglês
Publicado em: MDPI AG 2025-07-01
coleção:Applied Sciences
Assuntos:
rudder shaft
thermal protection
active cooling
phase change
structure optimized design
Acesso em linha:https://www.mdpi.com/2076-3417/15/14/8105
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