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    Fluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional Intake

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005::page 04025056-1
    Author:
    Yuan Lin
    ,
    Chibing Shen
    ,
    Chenglong Wang
    ,
    Mingbo Sun
    ,
    Dongcai Tan
    ,
    Ang Su
    ,
    Banglei Guan
    ,
    Zhang Li
    ,
    Minggang Wan
    DOI: 10.1061/JAEEEZ.ASENG-6143
    Publisher: American Society of Civil Engineers
    Abstract: This study aims to enhance the verification database for fluid–thermal–structural interaction (FTSI) experiments and develop a comprehensive methodology for parameter measurement in such tests. A complex S-shaped wedge model was selected to perform a 40-s FTSI experiment, and the effects of varying Mach numbers (Ma∞) on FTSI were analyzed using a validated numerical code. The results confirm the feasibility of the experimental approach, demonstrating that the proposed method captures temporal variations in key parameters and verifies the accuracy of the custom-developed simulation code. The results show that although the S-shaped wedge experiences significant parameter changes during the initial phase of the test, these parameters stabilize at different times rather than concurrently. Furthermore, an increase in Mach number (Ma∞) intensifies FTSI effects, resulting in higher component temperatures, accelerated achievement of steady-state conditions, increased temperature gradients within components, greater structural deformation, and more pronounced variations in wall pressure distribution. It is suggested that increasing Ma∞ in future FTSI experiments will amplify observable phenomena, providing more pronounced insights into the interaction dynamics.
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      Fluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional Intake

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4307086
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    contributor authorYuan Lin
    contributor authorChibing Shen
    contributor authorChenglong Wang
    contributor authorMingbo Sun
    contributor authorDongcai Tan
    contributor authorAng Su
    contributor authorBanglei Guan
    contributor authorZhang Li
    contributor authorMinggang Wan
    date accessioned2025-08-17T22:32:45Z
    date available2025-08-17T22:32:45Z
    date copyright9/1/2025 12:00:00 AM
    date issued2025
    identifier otherJAEEEZ.ASENG-6143.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307086
    description abstractThis study aims to enhance the verification database for fluid–thermal–structural interaction (FTSI) experiments and develop a comprehensive methodology for parameter measurement in such tests. A complex S-shaped wedge model was selected to perform a 40-s FTSI experiment, and the effects of varying Mach numbers (Ma∞) on FTSI were analyzed using a validated numerical code. The results confirm the feasibility of the experimental approach, demonstrating that the proposed method captures temporal variations in key parameters and verifies the accuracy of the custom-developed simulation code. The results show that although the S-shaped wedge experiences significant parameter changes during the initial phase of the test, these parameters stabilize at different times rather than concurrently. Furthermore, an increase in Mach number (Ma∞) intensifies FTSI effects, resulting in higher component temperatures, accelerated achievement of steady-state conditions, increased temperature gradients within components, greater structural deformation, and more pronounced variations in wall pressure distribution. It is suggested that increasing Ma∞ in future FTSI experiments will amplify observable phenomena, providing more pronounced insights into the interaction dynamics.
    publisherAmerican Society of Civil Engineers
    titleFluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional Intake
    typeJournal Article
    journal volume38
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-6143
    journal fristpage04025056-1
    journal lastpage04025056-13
    page13
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
    contenttypeFulltext
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