首页> 外文期刊>International journal of hydrogen energy >A comparative study of highly underexpanded nitrogen and hydrogen jets using large eddy simulation
【24h】

A comparative study of highly underexpanded nitrogen and hydrogen jets using large eddy simulation

机译:使用大涡模拟对高度膨胀不足的氮气和氢气射流的比较研究

获取原文
获取原文并翻译 | 示例
       

摘要

Three-dimensional large eddy simulations (LES) of highly underexpanded hydrogen and nitrogen jets at the same nozzle pressure ratio (NPR) of 5.60 and at a Reynolds number around 105 are performed. The classical near-field structures of highly underexpanded jets are well captured by LES, especially the shape and size of Mach barrel for both jets are very similar and agree well with the available literature data. However, the flow field and the shock structures after the Mach disk differ significantly. The density in the annular shear layer of H-2 jet is much lower because of its smaller molecular weight. Meanwhile, the H-2 jet has a much longer jet core and more shock cells. The dominant instability mode is helical for the N-2 jet, but is axisymmetric for the H-2 jet. There are two discrete peaks of f(s) = 37.086 kHz and f(2s) = 45.695 kHz in the spectrum of the N-2 jet, while the spectrum of the H-2 jet is characterized by a fundamental screech frequency of f(s) = 47.020 kHz and its high-order harmonics. The H-2 jet mixes more rapidly with the ambient air but has a much smaller mixing area on cross-section planes. Mixing between the ambient air and fuel still takes places at the jet boundary defined according to the mixture fraction of Z = 0.02, and the area of fully turbulent region of the highly underexpanded jets seems to be less predicted based on the traditional vorticity T/NT (turbulenton-turbulent) interface for both jets. Copyright (C) 2016, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.
机译:在相同的喷嘴压力比(NPR)为5.60且雷诺数约为105的情况下,对高度未充分膨胀的氢气和氮气流进行了三维大涡模拟(LES)。 LES很好地捕获了高度未充分膨胀的射流的经典近场结构,尤其是两种射流的马赫枪管的形状和尺寸都非常相似,并且与现有文献数据相吻合。但是,马赫盘之后的流场和激波结构明显不同。 H-2射流的环形剪切层中的密度较低,因为其分子量较小。同时,H-2喷气机具有更长的喷气机核心和更多的冲击单元。对于N-2射流,主要的不稳定性模式是螺旋形的,而对于H-2射流,则是不对称的。 N-2射流的频谱中有两个离散峰f(s)= 37.086 kHz和f(2s)= 45.695 kHz,而H-2射流的频谱的特征在于基本的尖叫频率f( s)= 47.020 kHz及其高阶谐波。 H-2射流与环境空气的混合速度更快,但在横截面上的混合面积小得多。仍然在根据Z = 0.02的混合比定义的射流边界处发生环境空气和燃料之间的混合,并且根据传统的涡度T / NT似乎很难预测高度膨胀不足的射流的完全湍流区域的面积。两个喷嘴的(湍流/非湍流)界面。 Hydrogen Energy Publications,LLC(C)2016版权所有。由Elsevier Ltd.出版。保留所有权利。

著录项

  • 来源
    《International journal of hydrogen energy》 |2016年第9期|5151-5161|共11页
  • 作者单位

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

    Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Scramjet; Hydrogen; Highly underexpanded jet; Large eddy simulation;

    机译:超燃冲压发动机;氢;高度膨胀不足的喷射;大涡模拟;
  • 入库时间 2022-08-18 00:20:10

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号