Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows

doi:10.1016/j.actaastro.2020.03.004

CORC > 力学研究所 > 中国科学院力学研究所 > 流固耦合系统力学重点实验室(2012-)

	Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows
	Ju SJ 3; Sun ZX(孙振旭)3; Yang GW(杨国伟)3; Prapamonthon P 2,3; Zhang JY 1
刊名	ACTA ASTRONAUTICA
	2020-06-01
卷号	171 页码:300-310
关键词	Computational fluid dynamics Drag reduction Supersonic flow Energy deposition Opposing jet
ISSN号	0094-5765
DOI	10.1016/j.actaastro.2020.03.004
通讯作者	Sun, Zhenxu(sunzhenxu@imech.ac.cn)
英文摘要	The drag reduction characteristics play an important role in the supersonic vehicle design phase. According to two drag reduction schemes, the opposing jet and the upstream energy deposition have aroused the widespread interest of researchers. In the current study, the drag reduction effectiveness of a blunt body with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows is investigated numerically. The three-dimensional coupled implicit compressible Reynolds Averaged Navier-Stokes (RANS) equations coupled with the Menter's shear stress transport (SST) turbulence model are applied to numerically predict flow fields of the blunt body, the variance analysis method is introduced to a parametric study on the drag reduction. Results indicate that a larger overall drag is decreased by the combinational configuration than the single strategies of the opposing jet and the energy deposition. The proposal of the combination of the upstream energy deposition and the opposing jet configuration can be used as an effective method of drag reduction. Meanwhile, due to the existence of the upstream energy deposition, the stability and penetrability of the opposing jet substantially increase, especially for the long penetration mode. Further, some recommendations are provided for the drag reduction factor and drag reduction effectiveness.
分类号	二类/Q1
资助项目	Postdoctoral Project for Advanced Engineering Construction of the Chinese Academy of Sciences
WOS关键词	HEAT-FLUX REDUCTION ; PULSED COUNTERFLOWING JET ; THERMAL PROTECTION SYSTEM ; BLUNT-BODY ; DESIGN EXPLORATION ; NUMERICAL SIMULATIONS ; HYPERSONIC FLOW ; MECHANISM ; CAVITY ; SPIKE
WOS研究方向	Engineering
语种	英语
WOS记录号	WOS:000524257600026
资助机构	Postdoctoral Project for Advanced Engineering Construction of the Chinese Academy of Sciences
其他责任者	Sun, Zhenxu
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/81867]
专题	力学研究所_流固耦合系统力学重点实验室(2012-)
作者单位	1.Shenyang Aerosp Univ, Sch Aerosp Engn, Shenyang 110136, Peoples R China 2.Int Acad Aviat Ind, King Mongkuts Inst Technol Ladkrabang, Bangkok 10520, Thailand; 3.Chinese Acad Sci, Key Lab Mech Fluid Solid Coupling Syst, Inst Mech, Beijing 100190, Peoples R China;
推荐引用方式 GB/T 7714	Ju SJ,Sun ZX,Yang GW,et al. Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows[J]. ACTA ASTRONAUTICA,2020,171:300-310.
APA	Ju SJ,孙振旭,杨国伟,Prapamonthon P,&Zhang JY.(2020).Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows.ACTA ASTRONAUTICA,171,300-310.
MLA	Ju SJ,et al."Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows".ACTA ASTRONAUTICA 171(2020):300-310.