| Computational-Fluid-Dynamics Solver with Preconditioned Method for Aerodynamic Simulation of High-Lift Configuration | |
Liu ZY(刘中玉) ; Liu W; Nie XY(聂雪媛); Yang GW(杨国伟); Liu, ZY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
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| Source Publication | JOURNAL OF AIRCRAFT
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| 2016 | |
| Volume | 53Issue:4Pages:1056-1064 |
| ISSN | 0021-8669 |
| Abstract | Apreconditioned method with characteristic boundary conditions for Navier-Stokes equations is implemented for flowfield analysis of a high-lift configuration at low Mach number. A preconditioned Harten-Lax-van Leer-Einfeldt-Wada scheme is adopted for the spatial discretization, and the dissipation term of which is rededuced to reduce the overlarge numerical dissipation. Preconditioned characteristic boundary conditions for the far field are derived based on the Weiss-Smith preconditioner and are demonstrated to be more reliable and accurate when coupled with the preconditioned method. Apreconditioned Lower-Upper Symmetric Gauss-Seidel implicit time-marching method is modified according to the preconditioned Jacobian matrix. The applications of the current method on both two- and three-dimensional high-lift configurations indicate that the use of the preconditioned spatial and time discrete schemes and the derived preconditioned characteristic boundary conditions is capable of improving the robustness, efficiency, and accuracy of the computational-fluid-dynamics solver for low-Mach-number aerodynamic simulations. |
| DOI | 10.2514/1.C033612 |
| URL | 查看原文 |
| Indexed By | SCI ; EI |
| Language | 英语 |
| WOS ID | WOS:000384297100017 |
| WOS Research Area | Engineering |
| WOS Subject | Engineering, Aerospace |
| Funding Organization | This work was supported by the National High-Tech Research and Development Program of China 2014AA110501. |
| Department | LMFS流固耦合与数值计算(LHO) |
| Classification | 二类 |
| Ranking | True |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/59717 |
| Collection | 流固耦合系统力学重点实验室 |
| Corresponding Author | Liu, ZY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China. |
| Recommended Citation GB/T 7714 | Liu ZY,Liu W,Nie XY,et al. Computational-Fluid-Dynamics Solver with Preconditioned Method for Aerodynamic Simulation of High-Lift Configuration[J]. JOURNAL OF AIRCRAFT,2016,53,4,:1056-1064. |
| APA | 刘中玉,Liu W,聂雪媛,杨国伟,&Liu, ZY .(2016).Computational-Fluid-Dynamics Solver with Preconditioned Method for Aerodynamic Simulation of High-Lift Configuration.JOURNAL OF AIRCRAFT,53(4),1056-1064. |
| MLA | 刘中玉,et al."Computational-Fluid-Dynamics Solver with Preconditioned Method for Aerodynamic Simulation of High-Lift Configuration".JOURNAL OF AIRCRAFT 53.4(2016):1056-1064. |
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| a2016-082.pdf（783KB） | 期刊论文 | 作者接受稿 | 开放获取 | CC BY-NC-SA | View Download | |
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