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大射电望远镜FAST风环境数值模拟研究
引用本文:吴明长,王启明,郭永卫,赵保庆. 大射电望远镜FAST风环境数值模拟研究[J]. 天文研究与技术, 2012, 0(2): 121-128,149
作者姓名:吴明长  王启明  郭永卫  赵保庆
作者单位:中国科学院国家天文台
基金项目:国家自然科学基金(11173035);国家天文台青年人才基金项目资助
摘    要:500 m口径球面射电望远镜(Five-hundred-meter Aperture Spherical radio Telescope,FAST),整体结构处于复杂的喀斯特地貌上,反射面承受风载荷作用,需要进行抗风设计。建立了FAST反射面及其周边山地地形的计算流体动力学(Computational Fluid Dynamics,CFD)计算模型,计算域范围为40 km×10 km×5.5 km。确定了入口风速剖面的基准高度为海拔810 m。计算了不同风向下反射面风压系数分布特征,得出了不利风向。对挡风墙的研究结果表明,挡风墙高度选择的效果优于位置选择。该研究结果可为FAST工程提供抗风设计的初步参考。

关 键 词:风载荷  抗风设计  数值模拟  计算流体动力学  风压系数  气动系数  挡风墙

A Numerical Study on the Wind Environment of the FAST
Wu Mingchang,Wang Qiming,Guo Yongwei,Zhao Baoqing. A Numerical Study on the Wind Environment of the FAST[J]. Astronomical Research & Technology, 2012, 0(2): 121-128,149
Authors:Wu Mingchang  Wang Qiming  Guo Yongwei  Zhao Baoqing
Affiliation:(National Astronomical Observatories,Chinese Academy of Sciences,Beijing 100012,China)
Abstract:The main structure of the Five-hundred-meter Aperture Spherical radio Telescope(FAST) will be constructed in a complex Karst landform.The FAST primary reflector will have to function with the presence of wind load.A wind-resistant design is necessary for the FAST.Currently,the field-test,wind-tunnel test,and numerical-simulation approaches are the three main methods to acquire the wind-pressure coefficients.Normally,a field test is not economic either in labor cost or financial expense.A wind-tunnel test is also expensive.For this study,numerical simulations are chosen for a preliminary study.Any field test will be performed in future if necessary.We construct certain geometric models,mesh models,and CFD(Computational Fluid Dynamics) analysis models for the FAST reflector and its surrouding terrains.The CFD models are built for the FAST reflector and the surrounding landform within 40km × 10km × 5.5km.A reference altitude of 810m is used for the profile of wind velocity at the inlet.We use the model to investigate the pressure coefficients of the reflector for different wind directions.For a panel of 35.4% perforation rate,we perform numerical analyses to acquire the relation between wind speed and pressure drop across the panel.The calculated aerodynamic coefficients are consistent with previous screen test results within 3%.Combining with porous jump boundary conditions,we use the methods to simulate the aerodynamic performance of the FAST reflector.We obtain the distributions of the wind pressure coefficients for multiple wind directions.The results show that the wind direction is a major factor and at the 5.5 o’ clock direction wind can have the most sever effects.Our simulation results show that the choice of windbreak height is of more importance than the choice of windbreak position.The results can be used as references for the wind-resistant design of the FAST,the subsequent construction procedure,and the high-precision measurement and control of the FAST reflector.
Keywords:Wind load  Wind-resistant design  Numerical simulation  Computational Fluid Dynamics  Pressure coefficient  Aerodynamic coefficient  Windbreak
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