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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Autors principals:	Xiangchun Sun, Kaiyan Jin, Kuan Zhao, Hexuan Zhang, Guice Yao, Dongsheng Wen
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2025-07-01
Col·lecció:	Applied Sciences
Matèries:	rudder shaft thermal protection active cooling phase change structure optimized design
Accés en línia:	https://www.mdpi.com/2076-3417/15/14/8105
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