Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV

doi:10.1186/s42774-021-00082-x

CORC > 力学研究所 > 中国科学院力学研究所 > 高温气体动力学国家重点实验室

	Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
	Qi H(齐涵)2,3; Li XL(李新亮)2,3; Yu ZP(于长平)3; Tong FL(童福林)1,3
刊名	Advances in Aerodynamics
	2021-10-08
卷号	3 期号:1
关键词	Lifting body model Hypersonic transition Direct numerical simulation
DOI	10.1186/s42774-021-00082-x
通讯作者	Li,Xinliang(lixl@imech.ac.cn) ; Yu,Changping(cpyu@imech.ac.cn)
英文摘要	AbstractDirect numerical simulation (DNS) of transition over a hypersonic lifting body model HyTRV developed by China Aerodynamics Research and Development Center is performed. The free-stream parameters are: the free-stream Mach number is 6, the unit Reynolds number is 10000/mm, the free-stream temperature is 79?K, the?angle of attack is 0, and the wall temperature is 300?K. Weak random blowing-and-suction perturbations in the leading range are used to trigger the transition. A high order finite-difference code OpenCFD developed by the authors is used for the simulation, and grid convergence test shows that the transition locations are grid-convergence. DNS results show that transition occurs in central area of the lower surface and the concaved region of the upper surface, and the transition regions are also the streamline convergence regions. The transition mechanisms in different regions are investigated by using the?spectrum and POD analysis.
语种	英语
WOS记录号	BMC:10.1186/S42774-021-00082-X
其他责任者	Li,Xinliang ; Yu,Changping
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/87534]
专题	力学研究所_高温气体动力学国家重点实验室
作者单位	1.China Aerodynamics Research and Development Center; Computational Aerodynamics Institute 2.University of Chinese Academy of Sciences; School of Engineering Science; 3.Institute of Mechanics, Chinese Academy of Sciences; State Key Laboratory of High Temperature Gas Dynamics;
推荐引用方式 GB/T 7714	Qi H,Li XL,Yu ZP,et al. Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV[J]. Advances in Aerodynamics,2021,3(1).
APA	齐涵,李新亮,于长平,&童福林.(2021).Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV.Advances in Aerodynamics,3(1).
MLA	齐涵,et al."Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV".Advances in Aerodynamics 3.1(2021).