Fluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional IntakeSource: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005::page 04025056-1Author:Yuan Lin
,
Chibing Shen
,
Chenglong Wang
,
Mingbo Sun
,
Dongcai Tan
,
Ang Su
,
Banglei Guan
,
Zhang Li
,
Minggang Wan
DOI: 10.1061/JAEEEZ.ASENG-6143Publisher: 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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| contributor author | Yuan Lin | |
| contributor author | Chibing Shen | |
| contributor author | Chenglong Wang | |
| contributor author | Mingbo Sun | |
| contributor author | Dongcai Tan | |
| contributor author | Ang Su | |
| contributor author | Banglei Guan | |
| contributor author | Zhang Li | |
| contributor author | Minggang Wan | |
| date accessioned | 2025-08-17T22:32:45Z | |
| date available | 2025-08-17T22:32:45Z | |
| date copyright | 9/1/2025 12:00:00 AM | |
| date issued | 2025 | |
| identifier other | JAEEEZ.ASENG-6143.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4307086 | |
| description 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. | |
| publisher | American Society of Civil Engineers | |
| title | Fluid–Thermal–Structural Interactions on a Supersonic Two-Dimensional Intake | |
| type | Journal Article | |
| journal volume | 38 | |
| journal issue | 5 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-6143 | |
| journal fristpage | 04025056-1 | |
| journal lastpage | 04025056-13 | |
| page | 13 | |
| tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 005 | |
| contenttype | Fulltext |