Effect of tunnel cross section on gas temperatures and heat fluxes in case of large heat release rate

被引:56
作者
Fan, Chuan Gang [1 ]
Li, Ying Zhen [2 ]
Ingason, Haukur [2 ]
Lonnermark, Anders [2 ]
机构
[1] Hefei Univ Technol, Sch Transportat Engn, Hefei, Peoples R China
[2] SP Tech Res Inst Sweden, Fire Res, Boras, Sweden
基金
中国国家自然科学基金; 瑞典研究理事会;
关键词
Model scale; Tunnel cross section; Gas temperature; Heat flux; Longitudinal ventilation; LONGITUDINAL VENTILATION; NATURAL VENTILATION; CEILING JET; AIR-FLOW; FIRE; FLAME; VELOCITY; MODEL; COMPARTMENT; STAIRWELL;
D O I
10.1016/j.applthermaleng.2015.09.048
中图分类号
O414.1 [热力学];
学科分类号
摘要
Tests with liquid and solid fuels in model tunnels (1:20) were performed and analysed in order to study the effect of tunnel cross section (width and height) together with ventilation velocity on ceiling gas temperatures and heat fluxes. The model tunnel was 10 m long with varying width (0.3 m, 0.45 m and 0.6 m) and height (0.25 m and 0.4 m). Test results show that the maximum temperature under the ceiling is a weak function of heat release rate (HRR) and ventilation velocity for cases with HRR more than 100 MW at full scale. It clearly varies with the tunnel height and is a weak function of the tunnel width. With a lower tunnel height, the ceiling is closer to the base of continuous flame zone and the temperatures become higher. Overall, the gas temperature beneath the ceiling decreases with the increasing tunnel dimensions, and increases with the increasing longitudinal ventilation velocity. The HRR is also an important factor that influences the decay rate of excess gas temperature, and a dimensionless HRR integrating HRR and other two key parameters, tunnel cross-sectional area and distance between fuel centre and tunnel ceiling, was introduced to account for the effect. An equation for the decay rate of excess gas temperature, considering both the tunnel dimensions and HRR, was developed. Moreover, a larger tunnel cross-sectional area will lead to a smaller heat flux. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:405 / 415
页数:11
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