AEROSPACE SHANGHAI, Volume. 41, Issue 4, 11(2024)
Analysis on Heat Transfer Characteristics of Film-based Structures with Temperature Sensitive Paint in Hypersonic Wind Tunnels
Fig. 1. The relationship between the minimum applicable thickness of typical model materials and the running time
Fig. 2. Surface and internal heat transfer characteristics of the stainless steel under typical flow field conditions
Fig. 3. The comparison between the numerical and theoretical solutions of stainless steel surface temperature rise under typical flow field conditions
Fig. 4. The relationship between the internal thermal diffusion depth of model materials and the surface heat flux under typical flow field conditions
Fig. 5. Surface and internal heat transfer characteristics of the film-based structure under typical flow field conditions
Fig. 6. The relationship between the internal thermal diffusion depth of film-based structures and the surface heat flux under typical flow field conditions
Fig. 7. The relationship between the internal thermal diffusion depth of film-based structures and the TSP thickness under typical flow field conditions
Fig. 8. The relationship between the surface temperature rise of model materials and the surface heat flux under typical flow field conditions
Fig. 9. The relationship between the surface temperature rise of film-based structures and the surface heat flux under typical flow field conditions
Fig. 10. The relationship between the surface temperature rise of film-based structures and the TSP thickness under typical flow field conditions
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Yanheng ZHANG, Yu ZHUANG, Dong ZHI, Shouchao HU, Tao JIANG. Analysis on Heat Transfer Characteristics of Film-based Structures with Temperature Sensitive Paint in Hypersonic Wind Tunnels[J]. AEROSPACE SHANGHAI, 2024, 41(4): 11
Category: Aerospace Aerodynamics and Test Technology
Received: Jan. 4, 2024
Accepted: --
Published Online: Nov. 18, 2024
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