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Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows
Lee YC(李亚超)1,2; Yao W(姚卫)1,2; Fan XJ(范学军)1,2
Source PublicationAIAA JOURNAL
2018-08-01
Volume56Issue:8Pages:3086-3096
ISSN0001-1452
Abstract

To reduce the numerical dissipation in turbulence modeling while maintaining the numerical stability around flow discontinuities in supersonic flowfield, a low-dissipative compressible solver is developed for large-eddy simulation within the OpenFOAM framework. To achieve the aforementioned goals, the low-dissipative solver adopts the hybrid scheme approach through combining the dissipative Kurganov-Tadmor scheme with the nondissipative central scheme via a shock sensor. In the construction of the central scheme, a robust skew-symmetric form of the convective term is adopted to preserve the local kinetic energy without adding an explicit dissipative term. Another feature of the low-dissipative solver is the implementation of an optimal explicit strong stability-preserving linear third-order total variation diminishing Runge-Kutta method for the temporal discretization. Numerical tests for a series of canonical flow problems are carried out to validate the solver's good performance in the flowfield either with strong discontinuities or with continuous spectrum characteristics. Large-eddy simulation of a scramjet combustor with supersonic airstream passing over the flame holder is conducted to validate the low-dissipative solver's reliability in a realistic flow with the complex interaction of shock discontinuities and turbulence.

DOI10.2514/1.J056404
Indexed BySCI ; EI
Language英语
WOS IDWOS:000440402900012
WOS KeywordHyperbolic Conservation-laws ; Navier-stokes Equations ; Shock-capturing Schemes ; Efficient Implementation ; Boundary-layers ; Formulations ; Stability ; Model
WOS Research AreaEngineering
WOS SubjectEngineering, Aerospace
Funding OrganizationNational Natural Science Foundation of China(11502270) ; Training Program of the Major Research Plan of the National Natural Science Foundation of China(91641110)
Classification一类/力学重要期刊
Ranking1
Citation statistics
Cited Times:1[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/77648
Collection高温气体动力学国家重点实验室
Corresponding AuthorYao W(姚卫); Fan XJ(范学军)
Affiliation1.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China
2.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
Recommended Citation
GB/T 7714
Lee YC,Yao W,Fan XJ. Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows[J]. AIAA JOURNAL,2018,56(8):3086-3096.
APA Lee YC,Yao W,&Fan XJ.(2018).Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows.AIAA JOURNAL,56(8),3086-3096.
MLA Lee YC,et al."Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows".AIAA JOURNAL 56.8(2018):3086-3096.
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