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dc.contributor.authorYuan Lin
dc.contributor.authorChibing Shen
dc.contributor.authorChenglong Wang
dc.contributor.authorMingbo Sun
dc.contributor.authorDongcai Tan
dc.contributor.authorAng Su
dc.contributor.authorBanglei Guan
dc.contributor.authorZhang Li
dc.contributor.authorMinggang Wan
dc.date.accessioned2025-08-17T22:32:45Z
dc.date.available2025-08-17T22:32:45Z
dc.date.copyright9/1/2025 12:00:00 AM
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-6143.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307086
dc.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.
dc.publisherAmerican Society of Civil Engineers
dc.titleFluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional Intake
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue5
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6143
dc.journal.fristpage04025056-1
dc.journal.lastpage04025056-13
dc.page13
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005
dc.contenttypeFulltext


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