CFD/DSMC 혼합해석기법을 이용한 축대칭 천이영역 유동 해석 Simulations of Axisymmetric Transition Flow Regimes Using a CFD/DSMC Hybrid Method

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In the present study, a CFD/DSMC hybrid method performed by a coupled analysis between the CFD method and the DSMC method was developed to obtain the flow information on the rarefied gas flows effectively. Flow simulations around the high speed vehicles on the transition flow regimes were conducted by using the developed method. The FRESH-FX vehicle made of cone and cylinder shapes was considered for the simulations. The results of the hybrid method were compared with the results of the pure CFD and the pure DSMC method to confirm the reliability and efficiency of the hybrid method. It was found that the gradient and the intensity of the shock waves were weakened due to the relatively low density on the transition flow regime. It was confirmed that the results of the hybrid analysis were different to those of the pure CFD analysis and almost identical to those of the pure DSMC analysis. In addition, the computational time of the hybrid method was reduced than that of the pure DSMC method. As a result, it was obtained that the validity and the efficiency of the CFD/DSMC hybrid method.
Publisher
KOREAN SOC AERONAUTICAL & SPACE SCIENCES
Issue Date
2019-03
Language
Korean
Article Type
Article
Citation

JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.47, no.3, pp.169 - 176

ISSN
1225-1348
DOI
10.5139/JKSAS.2019.47.3.169
URI
http://hdl.handle.net/10203/262089
Appears in Collection
AE-Journal Papers(저널논문)
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