...
首页> 外文期刊>Acta astronautica >Investigation of the evaporation characteristics of a transverse vaporized kerosene jet in supersonic flow
【24h】

Investigation of the evaporation characteristics of a transverse vaporized kerosene jet in supersonic flow

机译:超声波流动横向蒸发煤油射流蒸发特性的研究

获取原文
获取原文并翻译 | 示例
           

摘要

The distribution and evaporation characteristics of a transverse vaporized kerosene jet in supersonic flow were experimentally investigated in a ground direct-connected experimental system. Smear-free and high spatio-temporal resolution images of the jet plume were obtained using the pulsed laser sheet imaging method. The incoming flow had a total pressure of 1.0 MPa, a total temperature of 980 K, and an inlet Mach number of 2.0. The boundary and length of the jet plume were identified using the maximum interclass variance method (Otsu). The experimental results show that the kerosene evaporation process is closely related to the fuel temperature and local flow velocity. The two factors competitively influence the phase distribution in the jet plume, resulting in different evaporation distances in the direction perpendicular to the wall. Under subcritical conditions, the jet penetration depths remain basically constant, while the surface wave structures are distinct on the windward side. The jet of critical-state kerosene exhibits a quasi-gaseous flow structure in the near field and undergoes a complex phase transition of secondary condensation and secondary evaporation. According to the different phase states and evaporation degrees, the jet plume is divided into three evaporation regions, providing a complete description of the evaporation characteristics of kerosene at different temperatures in supersonic flow.
机译:在地面直接连接的实验系统中实验研究了超声波流动中横向蒸发煤油喷射的分布和蒸发特性。使用脉冲激光片成像方法获得喷射羽流的无涂片和高时空分辨率图像。进入的流量的总压力为1.0MPa,总温度为980 k,入口马赫数为2.0。使用最大杂机方差方法(OTSU)识别喷射羽流的边界和长度。实验结果表明,煤油蒸发过程与燃料温度和局部流速密切相关。这两个因素竞争地影响喷射羽流中的相位分​​布,从而导致垂直于墙壁的方向上的不同蒸发距离。在亚临界条件下,喷射渗透深度保持基本恒定,而表面波结构在迎风侧不同。临界状态煤油的射流在近场中表现出准气相结构,经历次级缩合和次级蒸发的复杂相转变。根据不同的相位状态和蒸发度,喷射羽流分成三个蒸发区域,提供超声波流动中不同温度下煤油的蒸发特性的完全描述。

著录项

  • 来源
    《Acta astronautica》 |2021年第8期|257-263|共7页
  • 作者单位

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

    Natl Univ Def Technol Sci & Technol Scramjet Lab Changsha 410073 Peoples R China;

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

    Scramjet; Vaporized kerosene; Transverse jet; Supersonic flow;

    机译:Scramjet;蒸发煤油;横向喷射;超音速流动;

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