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Numerical Analysis of Thermal Protection Structure of Aircraft Hood Considering Multi-field Coupling Effect |
LI Zongyang, LI Yu, CHENG Guangyi, DOU Yibin, ZHANG Xiaohong |
Shanghai Electro-Mechanical Engineering Institute |
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Abstract In order to use numerical analysis method more efficiently and accurately to study the multi-field coupling problem and fully consider the strong-weak coupling relationship between various physical fields, a multi-field coupling analysis method combining FVM with FEM is developed and applied to the numerical analysis of the thermal protection structure of the aircraft hood. The temperature and thermal deformation distribution inside the aircraft hood structure are obtained, which can provide reference for the thermal protection design of aircraft hood.
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Received: 03 September 2019
Published: 19 June 2020
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