Downburst wind field characteristics under moving effect

被引:0
|
作者
Wang Z. [1 ,2 ]
Wu Y. [1 ]
Fang Z. [1 ]
机构
[1] School of Civil Engineering, Chongqing University, Chongqing
[2] MOE Key Lab of Construction of Cities in Mountain Area and New Technology, Chongqing University, Chongqing
来源
关键词
Amplification effect; Jet velocity; Large eddy simulation; Translational velocity; Wind tunnel test;
D O I
10.13465/j.cnki.jvs.2019.03.005
中图分类号
学科分类号
摘要
Downburst wind field study under steady state is relatively mature. Due to storm moving, the actual downburst wind field is unsteady. In order to study effects of jet-flow velocity and translational velocity on characteristics of downburst wind field, a test for downburst wind field under moving was conducted with an impinging jet device. The large eddy simulation(LES) was used to build 3-D reduced scale and full-scale wind fields of impinging jet at moving nozzle to do numerical analysis. The results showed that the numerical simulation results agree well with test ones; moving speed has an obvious peak amplification action, and jet velocity has little effect on peak value; the translating downburst wind field has features of wind shift and obvious asymmetry, translating speed has a significant amplification effect on the horizontal wind speed near wall ahead of storm, but it causes some reduction in wind speed behind storm; when the downburst develops to enter a steady state, the wind profile increases to the maximum firstly and then decreases rapidly with increase in its height, the maximum wind speed appears at the lower end of the wind profile; the curve peak position and the duration of the curve descending segment are related to moving velocity and jet one in a certain proportion. © 2019, Editorial Office of Journal of Vibration and Shock. All right reserved.
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页码:32 / 38
页数:6
相关论文
共 22 条
  • [1] Fujita T.T., The downburst: Microburst and microburst, (1985)
  • [2] Proctor F.H., Numerical simulations of an isolated microburst. Part I: Dynamics and structure, Journal of the Atmospheric Sciences, 45, 21, pp. 3137-3160, (1988)
  • [3] Mason M.S., Wood G.S., Fletcher D.F., Influence of tile and surface roughness on the outflow wind field of an impinging jet, Wind and Structures an International Journal, 12, 12, pp. 179-204, (2009)
  • [4] Sengupta A., Sarkar P.P., Experimental measurement and numerical simulation of an impinging jet with application to thunderstorm microburst winds, Journal of Wind Engineering and Industrial Aerodynamics, 96, pp. 345-365, (2008)
  • [5] Vicroym D.A., Simple analytical axisymmetric microburst model for downdraft estimation, NASA Technical Memorandum, 104053, (1991)
  • [6] Li C., Li Q.S., Xiao Y.Q., Et al., A revised empirical model and CFD simulations for 3D axisymmetric steady-state flows of downbursts and impinging jets, Journal of Wind Engineering and Industrial Aerodynamics, 102, pp. 48-60, (2012)
  • [7] Zou X., Wang Z., Li Z., Study on the wind profile model of steady-state thunderstorm, Journal of Vibration and Shock, 35, 15, pp. 74-79, (2016)
  • [8] Oseguera R.M., Bowles R.L., A simple analytics 3-dimensi onal downburst model bason boundary layer stagnation flow, (1988)
  • [9] Wood G.S., Wok K.K.C.S., Motte Ram N.A., Et al., Physical and numerical modeling of thunderstorm downbursts, Journal of Wind Engineering and Industrial Aerodynamics, 89, 6, pp. 535-552, (2001)
  • [10] Vicroy D.D., Assessment of microburst models for downd-raft estimation, Journal of Aircraft, 29, (1992)