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Thermal protection system gap analysis using a loosely coupled fluid-structural thermal numerical method
- Source :
- Acta Astronautica. 146:368-377
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- A loosely coupled fluid-structural thermal numerical method is introduced for the thermal protection system (TPS) gap thermal control analysis in this paper. The aerodynamic heating and structural thermal are analyzed by computational fluid dynamics (CFD) and numerical heat transfer (NHT) methods respectively. An interpolation algorithm based on the control surface is adopted for the data exchanges on the coupled surface. In order to verify the analysis precision of the loosely coupled method, a circular tube example was analyzed, and the wall temperature agrees well with the test result. TPS gap thermal control performance was studied by the loosely coupled method successfully. The gap heat flux is mainly distributed in the small region at the top of the gap which is the high temperature region. Besides, TPS gap temperature and the power of the active cooling system (CCS) calculated by the traditional uncoupled method are higher than that calculated by the coupled method obviously. The reason is that the uncoupled method doesn't consider the coupled effect between the aerodynamic heating and structural thermal, however the coupled method considers it, so TPS gap thermal control performance can be analyzed more accurately by the coupled method.
- Subjects :
- 020301 aerospace & aeronautics
Materials science
business.industry
Numerical analysis
Aerodynamic heating
Aerospace Engineering
02 engineering and technology
Mechanics
Computational fluid dynamics
01 natural sciences
0203 mechanical engineering
Heat flux
Space Shuttle thermal protection system
0103 physical sciences
Heat transfer
Thermal
Active cooling
business
010303 astronomy & astrophysics
Subjects
Details
- ISSN :
- 00945765
- Volume :
- 146
- Database :
- OpenAIRE
- Journal :
- Acta Astronautica
- Accession number :
- edsair.doi...........e4123e9a5e0605bf4c09dfab1ae74549
- Full Text :
- https://doi.org/10.1016/j.actaastro.2018.02.047