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地铁站台活塞风附壁射流起始段的实测和实验验证
引用本文:王丽慧,杜晓明,任俊,韩星,龚伟,宋洁,姜昕.地铁站台活塞风附壁射流起始段的实测和实验验证[J].制冷学报,2014(3):65-70.
作者姓名:王丽慧  杜晓明  任俊  韩星  龚伟  宋洁  姜昕
作者单位:上海理工大学环境与建筑学院;上海申通轨道交通研究咨询有限公司;
基金项目:国家自然科学基金(50908147,51208298)资助项目;上海市教委重点学科建设项目(J50502);上海市大学生创新实验项目(SH1110252104)资助~~
摘    要:为了从机理上探究站台活塞风分布规律,通过理论建模、现场实测和液体缩尺模型实验相结合的方法,提出并验证了站台活塞风起始段符合附壁射流理论模型。其中,对上海某地铁站台层的现场实测较好验证了站台活塞风起始段自由剪切区的理论模型,理论与实测数据的标准差在0.326和0.542之间;液体缩尺模型实验对站台活塞风起始段边界层区、势流核心区和自由剪切区理论模型进行了验证,三区吻合较好,标准差在0.071和0.746之间。上述研究证明了站台活塞风附壁射流理论起始段的正确性。

关 键 词:站台活塞风  附壁射流起始段  现场实测  液体缩尺模型实验

The Field Measurement and Experimental Verification of Subway Platform Piston Wind Attached Jet Theory
Wang Lihui,Du Xiaoming,Ren Jun,Han Xing,Gong Wei,Song Jie and Jiang Xing.The Field Measurement and Experimental Verification of Subway Platform Piston Wind Attached Jet Theory[J].Journal of Refrigeration,2014(3):65-70.
Authors:Wang Lihui  Du Xiaoming  Ren Jun  Han Xing  Gong Wei  Song Jie and Jiang Xing
Affiliation:University of Shanghai for Science and Technology;University of Shanghai for Science and Technology;University of Shanghai for Science and Technology;University of Shanghai for Science and Technology;Shanghai Shentong Rail Transit Research Consulting Co., Ltd.;Shanghai Shentong Rail Transit Research Consulting Co., Ltd.;University of Shanghai for Science and Technology
Abstract:To study the platform piston wind distribution characteristics from the mechanism, it is put forward that the characteristics of platform piston wind conform to the attached jet theory, combining the theory modeling, field measurement and liquid scale model test. Based on the field measurement in a subway station in Shanghai, the field test data fit well with the theory calculation results in the initial segment of platform piston wind. The standard deviation between theory calculation and field measurement is between 0.326 and 0.542. The liquid scale model test is set up to verify the related mathematical model during the boundary layer district, potential flow core area and free shear zone in the initial segment. The model test results have good agreement with theory calculation with the standard deviation between 0.071 and 0.746. It is proved by above research works that the platform piston wind could be taken as the attached jet initial segment.
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