IMECH-IR  > 高温气体动力学国家重点实验室
Numerical investigation of characteristic frequency excited highly underexpanded jets
Li XP; Fan E; Yao W(姚卫); Fan XJ(范学军); Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.; Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
发表期刊AEROSPACE SCIENCE AND TECHNOLOGY
2017-04-01
卷号63页码:304-316
ISSN1270-9638
摘要

A highly underexpanded jet with a nozzle pressure ratio of 5.60 is excited simultaneously by the inherent characteristic frequencies in the steady jet of 14.569 kHz 37.086 kHz and 45.695 kHz as well as other two reference frequencies of 1.0 kHz and 40.0 kHz. The flow characteristic of the excited jets is revealed by comparing to the steady jet using large eddy simulation technique. For low-frequency excitation (fe = 1.0 kHz) the flow and acoustic fields of the forcing jet are similar with the steady jet. However when the jet is excited by high frequencies the acoustic source moves to the nozzle exit and the jet potential core together with the near-field shocks oscillate periodically at the excitation frequency. The excitation at fe = 1.0 kHz increases the mixing area since y/D = 24 from the nozzle exit which is contrary to the effect of other high frequencies that enhances the mixing in the near-field region but decreases the mixing area since y/D = 18. The peak frequency of the excited jets generally becomes identical to the excitation frequency once being excited except the fe = 1.0 kHz and h = 40.0 kHz jets. High-order harmonics of the dominant frequency are observed in the pressure spectrum of jets excited by high frequencies and the dominant mode turns into the axisymmetric mode from the original helical one accordingly. In particular forcing the jet with the axisymmetric mode of h = 14.569 kHz provides the fewest shock cells but the largest amplitude in shock oscillation the most harmonics in the spectrum and the largest mixing area within 8 < y/D < 12. 2017 Elsevier Masson SAS. All rights reserved.

关键词Fuel Jets Underexpanded Jets Jet Mixing Control Excited Jets Large Eddy Simulation
DOI10.1016/j.ast.2017.01.005
收录类别SCI ; EI
语种英语
WOS记录号WOS:000395960200029
关键词[WOS]LARGE-EDDY SIMULATION ; SUPERSONIC JET ; CROSS-FLOW ; PULSED JETS ; CENTRAL SCHEMES ; TRANSVERSE JET ; CIRCULAR JETS ; HIGH-SPEED ; INJECTOR ; CONFIGURATION
WOS研究方向Engineering
WOS类目Engineering, Aerospace
项目资助者National Natural Science Foundation of China(11502270) ; China Postdoctoral Science Foundation(2016M591258)
课题组名称LHD超声速燃烧
论文分区一类
力学所作者排名1
引用统计
被引频次:14[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/311007/60562
专题高温气体动力学国家重点实验室
通讯作者Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.; Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
推荐引用方式
GB/T 7714
Li XP,Fan E,Yao W,et al. Numerical investigation of characteristic frequency excited highly underexpanded jets[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2017,63:304-316.
APA Li XP,Fan E,姚卫,范学军,Fan, XJ ,&Fan, XJ .(2017).Numerical investigation of characteristic frequency excited highly underexpanded jets.AEROSPACE SCIENCE AND TECHNOLOGY,63,304-316.
MLA Li XP,et al."Numerical investigation of characteristic frequency excited highly underexpanded jets".AEROSPACE SCIENCE AND TECHNOLOGY 63(2017):304-316.
条目包含的文件 下载所有文件
文件名称/大小 文献类型 版本类型 开放类型 使用许可
JouAr-2017-059.pdf(3588KB)期刊论文作者接受稿开放获取CC BY-NC-SA浏览 下载
个性服务
推荐该条目
保存到收藏夹
查看访问统计
导出为Endnote文件
Lanfanshu学术
Lanfanshu学术中相似的文章
[Li XP]的文章
[Fan E]的文章
[姚卫]的文章
百度学术
百度学术中相似的文章
[Li XP]的文章
[Fan E]的文章
[姚卫]的文章
必应学术
必应学术中相似的文章
[Li XP]的文章
[Fan E]的文章
[姚卫]的文章
相关权益政策
暂无数据
收藏/分享
文件名: JouAr-2017-059.pdf
格式: Adobe PDF
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。