Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows | |
Ju SJ(鞠胜军)1; Sun ZX(孙振旭)1; Yang GW(杨国伟)1; Prapamonthon P1,2; Zhang JY3 | |
通讯作者 | Sun, Zhenxu(sunzhenxu@imech.ac.cn) |
发表期刊 | AEROSPACE SCIENCE AND TECHNOLOGY |
2020-10-01 | |
卷号 | 105页码:10 |
ISSN | 1270-9638 |
摘要 | Optimization design has been widely used in the supersonic vehicle design process and the drag reduction characteristic is an important objective of the optimization. The drag reduction mechanism applied to the blunt body with the combinational configuration of the upstream energy deposition and opposing jet for drag reduction has been conducted numerically. In the current study, the three-dimensional coupled implicit compressible Reynolds Averaged Navier-Stokes equations and Menter's shear stress transport turbulence model are employed to simulate the flow fields around the blunt body with the combined method. The results show that in the jet-to-freestream total-pressure ratio of 0.2 and 0.4, the drag is reduced by 47.44% and 45.96%, respectively. Further, the Latin hypercube method is used for the generation of initial samples for optimization and the multi-objective design optimization algorithm coupled with the Kriging model surrogate model is applied to determine optimal flow control parameters. The drag reduction factor R-d and drag reduction effectiveness E-eff are selected as optimization objectives. The Pareto-optimal front for the multi-objective design optimization results is acquired and there exists a challenging tradeoff between the two optimization objectives. The drag reduction factor R-d and drag reduction effectiveness E-eff further increase as much as 28.16% and 116.47%, respectively. The jet has a stronger penetration in the optimum design condition, and the findings suggest that the strategy of adding energy spot to the upstream flow field of the opposing jet can be an effective way for drag reduction. (C) 2020 Elsevier Masson SAS. All rights reserved. |
关键词 | Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
DOI | 10.1016/j.ast.2020.105941 |
收录类别 | SCI ; EI |
语种 | 英语 |
WOS记录号 | WOS:000573518200003 |
关键词[WOS] | TRANSVERSE HYDROGEN JET ; MICRO AIR-JETS ; CAVITY FLAMEHOLDER ; BLUNT-BODY ; MIXING AUGMENTATION ; COUNTERFLOWING JET ; HYPERSONIC FLOW ; HEAT-TRANSFER ; COEFFICIENT ; PERFORMANCE |
WOS研究方向 | Engineering |
WOS类目 | Engineering, Aerospace |
资助项目 | Postdoctoral Project for Advanced Engineering Construction of the Chinese Academy of Sciences |
项目资助者 | Postdoctoral Project for Advanced Engineering Construction of the Chinese Academy of Sciences |
论文分区 | 一类 |
力学所作者排名 | 1 |
RpAuthor | Sun, Zhenxu |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/85283 |
专题 | 流固耦合系统力学重点实验室 |
作者单位 | 1.Chinese Acad Sci, Key Lab Mech Fluid Solid Coupling Syst, Inst Mech, Beijing 100190, Peoples R China; 2.King Mongkuts Inst Technol Ladkrabang, Int Acad Aviat Ind, Dept Aeronaut Engn, Bangkok 10520, Thailand; 3.Shenyang Aerosp Univ, Sch Aerosp Engn, Shenyang 110136, Peoples R China |
推荐引用方式 GB/T 7714 | Ju SJ,Sun ZX,Yang GW,et al. Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2020,105:10. |
APA | 鞠胜军,孙振旭,杨国伟,Prapamonthon P,&Zhang JY.(2020).Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows.AEROSPACE SCIENCE AND TECHNOLOGY,105,10. |
MLA | 鞠胜军,et al."Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows".AEROSPACE SCIENCE AND TECHNOLOGY 105(2020):10. |
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