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Fluid flow characteristics of single inclined circular jet impingement for ultra-fast cooling
  • ISSN号:1671-833X
  • 期刊名称:《航空制造技术》
  • 时间:0
  • 分类:TQ051.13[化学工程] TK124[动力工程及工程热物理—工程热物理;动力工程及工程热物理—热能工程]
  • 作者机构:[1]State Key Laboratory of Rolling and Automation (Northeastern University), Shenyang 110819, China
  • 相关基金:Project(2010CB630800) supported by the National Basic Research Program of China; Project(N100307003) supported by the Fundamental Research Funds for the Central Universities, China
中文摘要:

The fluid flow characteristics of the single bunch inclined jet impingement were investigated with different jet flow velocities,nozzle diameters,jet angles and jet-to-target distances for ultra-fast cooling technology.The results show that the peak pressure varying significantly from nearly 0.5 to above 13.4 kPa locates at the stagnation point with different jet diameters,and the radius of impact pressure affected zone is small promoted from 46 to 81 mm in transverse direction,and 50 to 91 mm in longitude direction when the jet flow velocity changes from 5 to 20 m/s.However,the fluid flow velocity is relatively smaller near the stagnation point,and increases gradually along the radius outwards,then declines.There is an obvious anisotropic characteristic that the flow velocity component along the jet direction is about twice of the contrary one where the jet anlge is 60°,jet diameter is 5 mm,jet length is 8 mm and jet height is 50 mm.

英文摘要:

The fluid flow characteristics of the single bunch inclined jet impingement were investigated with different jet flow velocities, nozzle diameters, jet angles and jet-to-target distances for ultra-fast cooling technology. The results show that the peak pressure varying significantly from nearly 0.5 to above 13.4 kPa locates at the stagnation point with different jet diameters, and the radius of impact pressure affected zone is small promoted from 46 to 81 mm in transverse direction, and 50 to 91 mm in longitude direction when the jet flow velocity changes from 5 to 20 m/s. However, the fluid flow velocity is relatively smaller near the stagnation point, and increases gradually along the radius outwards, then declines. There is an obvious anisotropic characteristic that the flow velocity component along the jet direction is about twice of the contrary one where the jet anlge is 60°, jet diameter is 5 mm, jet length is 8 mm and jet height is 50 mm.

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期刊信息
  • 《航空制造技术》
  • 中国科技核心期刊
  • 主管单位:中国航空工业集团公司
  • 主办单位:北京航空制造工程研究所
  • 主编:刘柱
  • 地址:北京市朝阳区八里桥北东军庄1号
  • 邮编:100024
  • 邮箱:lzm@amte.net.cn
  • 电话:010-85700465
  • 国际标准刊号:ISSN:1671-833X
  • 国内统一刊号:ISSN:11-4387/V
  • 邮发代号:82-26
  • 获奖情况:
  • 中文核心期刊,中国科技论文统计用刊,中国期刊方阵“双百”期刊
  • 国内外数据库收录:
  • 中国中国科技核心期刊,中国北大核心期刊(2011版)
  • 被引量:10629