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作 者:邵树峰[1] 严俊杰[1] 曹岩[1] 刘继平[1]
机构地区:[1]西安交通大学动力工程多相流国家重点实验室,陕西西安710049
出 处:《工程热物理学报》2007年第1期68-70,共3页Journal of Engineering Thermophysics
基 金:国家自然科学基金资助项目(No.50676078);教育部新世纪优秀人才支持计划资助(No.NCET-04-0940)
摘 要:本文对压力为0.20-0.40 MPa的蒸汽在27℃环境水中超音速浸没射流与凝结换热进行了实验研究。实验与分析结果表明:流场分为汽羽、汽液界面、汽液两相混合区和环境水四个区域;随着蒸汽入口压力的增大,依次出现圆锥-椭圆双层汽羽、圆锥形汽羽和椭圆形汽羽;当蒸汽入口压力从0.20 MPa增大到0.40 MPa时,汽羽的无量纲穿透长度从2.20近似线性增大到4.20,射流平均凝结换热系数随着蒸汽入口压力的增大缓慢减小,其数值在0.67-0.80 MW/(m2·℃)之间变化。The flow and condensation heat transfer of supersonic steam jet immerged in subcool water was investigated experimentally. The inlet pressure of steam was at the range of 0.20~0.40 MPa and the temperature of subcool water was 27℃. The experimental and analytical results show that: the flow region consists of four different parts, namely steam plume, steam-water interface, steam-water mixing layer and pure water; With the increase of inlet steam pressure at the range of 0.20~0.40 MPa, there are three kinds of steam plume, namely conical-elliptical double layers, conical and elliptical steam plumes, and the non-dimension penetration length of steam plume linearly increases from 2.20 to 4.20 while the condensation heat transfer coefficient slowly decreases from 0.80 to 0.67 MW/(m2·℃).
分 类 号:TK2[动力工程及工程热物理—动力机械及工程]
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