Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows | |
Lee YC(李亚超)1,2![]() ![]() ![]() | |
Source Publication | AIAA JOURNAL
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2018-08-01 | |
Volume | 56Issue:8Pages:3086-3096 |
ISSN | 0001-1452 |
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. |
DOI | 10.2514/1.J056404 |
Indexed By | SCI ; EI |
Language | 英语 |
WOS ID | WOS:000440402900012 |
WOS Keyword | Hyperbolic Conservation-laws ; Navier-stokes Equations ; Shock-capturing Schemes ; Efficient Implementation ; Boundary-layers ; Formulations ; Stability ; Model |
WOS Research Area | Engineering |
WOS Subject | Engineering, Aerospace |
Funding Organization | National 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 |
Ranking | 1 |
Citation statistics | |
Document Type | 期刊论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/77648 |
Collection | 高温气体动力学国家重点实验室 |
Corresponding Author | Yao W(姚卫); Fan XJ(范学军) |
Affiliation | 1.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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