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Shock oscillation in highly underexpanded jets
Li XP; Zhou R; Chen XP; Fan XJ(范学军); Xie GS
发表期刊CHINESE PHYSICS B
2018-09-01
卷号27期号:9页码:94705
ISSN1674-1056
摘要

The oscillatory motions of shocks in highly underexpanded jets with nozzle pressure ratios of 5.60, 7.47, 9.34, and 11.21 are quantitatively studied by using large eddy simulation. Two types of shock oscillations are observed: one is the Mach disk oscillation in the streamwise direction and the other is the shock oscillation in the radial direction. It is found that the Mach disk moves quickly in the middle of the oscillatory region but slowly at the top or bottom boundaries. The oscillation cycles of Mach disk are the same for different cases, and are all dominated by an axisymmetric mode of 5.298 kHz. For the oscillation in the radial direction, the shocks oscillate more toward the jet centerline but less in the jet shear layer, and the oscillation magnitude is an increasing function of screech amplitude. The cycles of the radial shock oscillation switch randomly between the two screech frequencies for the first two cases. However, the oscillation periodicity is more complex for the jets with high nozzle pressure ratios of 9.34 and 11.21 than for the jets with the low nozzle pressure ratios of 5.6 and 7.47. In addition, the shock oscillation characteristics are also captured by coarse mesh and Smagorinsky model, but the coarse mesh tends to predict a slower and weaker shock oscillation.

关键词highly underexpanded jets shock oscillation large eddy simulation
DOI10.1088/1674-1056/27/9/094705
URL查看原文
收录类别SCI ; EI ; CSCD
语种英语
WOS记录号WOS:000445021100005
关键词[WOS]LARGE-EDDY SIMULATION ; UNDER-EXPANDED HYDROGEN ; SUPERSONIC JET ; METHANE JETS ; SCREECH ; NOISE ; PRESSURE ; ENGINES ; FLOWS ; FIELD
WOS研究方向Physics, Multidisciplinary
WOS类目Physics
项目资助者National Natural Science Foundation of China [11602028] ; Science and Technology Project of General Administration of Quality Supervision Inspection and Quarantine of China [2017QK119, 2017QK188]
CSCD记录号CSCD:6342848
论文分区Q3
力学所作者排名4
引用统计
被引频次:6[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://dspace.imech.ac.cn/handle/311007/77940
专题高温气体动力学国家重点实验室
作者单位1.China Special Equipment Inspect & Res Inst, Beijing 100029, Peoples R China
2.Inst Appl Phys & Computat Math, Lab Computat Phys, Beijing 100094, Peoples R China
3.Zhejiang Sci Tech Univ, Key Lab Fluid Transmiss Technol Zhejiang Prov, Hangzhou 310018, Zhejiang, Peoples R China
4.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Li XP,Zhou R,Chen XP,et al. Shock oscillation in highly underexpanded jets[J]. CHINESE PHYSICS B,2018,27,9,:94705.
APA Li XP,Zhou R,Chen XP,Fan XJ,&Xie GS.(2018).Shock oscillation in highly underexpanded jets.CHINESE PHYSICS B,27(9),94705.
MLA Li XP,et al."Shock oscillation in highly underexpanded jets".CHINESE PHYSICS B 27.9(2018):94705.
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