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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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