Simulation-driven Wind Load Analysis and Prediction for Large Steerable Radio Telescopes  

作　　者：Shuai Li Bao-Qing Han Shao-Yi Liu Wen-Juan Wang Ben-Ben Wang Xin-Yu Zhang Long-Yang Wang Qian Xu Na Wang Wu-Lin Zhao Cong-Si Wang 

机构地区：[1]Key Laboratory of Electronic Equipment Structure Design,Ministry of Education,Xidian University,Xi'an 710071,China [2]Xinjiang Astronomical Observatory,Chinese Academy of Sciences,Urumqi 830011,China [3]The 39th Research Institute of China Electronics Technology Group Corporation,Xi'an 710065,China [4]Guangzhou Institute of Technology,Xidian University,Guangzhou510555,China

出　　处：《Research in Astronomy and Astrophysics》2023年第2期18-27,共10页天文和天体物理学研究（英文版）

基　　金：supported by the National Key Research and Development Program of China(grant No.2021YFC2203600);the National Natural Science Foundation of China(Grant Nos.52275268 and 51975447);the National Defense Basic Scientific Research Program of China(Grant No.JCKY2021210B007);Wuhu and Xidian University Special Fund for Industry-University-Research Cooperation(Grant No.XWYCXY-012021012);Youth Innovation Team of Shaanxi Universities(Grant No.201926)。

摘　　要：Large steerable radio telescopes can rotate in azimuth and elevation,with various upwind postures and complex wind load characteristics.In order to obtain the wind load distribution on the reflector and the wind force coefficients in different upwind postures,this work took the reflector of the Qi Tai Telescope in Xinjiang as the object.The wind pressure distribution,drag coefficient,side force coefficient,lift coefficient,and total force coefficient of 361 groups of reflectors with different upwind postures were calculated and analyzed by a numerical simulation method.The results show that the force on the reflector when the concave surface faces the wind is significantly greater than when the convex surface faces the wind.The surrogate models for calculating wind force coefficients were established based on the polynomial response surface model(PRSM) and regularized minimumenergy tensor-product spline(RMTS).The adjusted R-squared of RMTS is 0.98,and the root mean square error is below 0.1,which proves RMTS is significantly better than PRSM.Compared with the numerical simulation values,the absolute errors of the drag coefficient,side force coefficient,lift coefficient,and total force coefficient of the reflector with azimuth and elevation of 45° predicted by RMTS are 0.02,0.027,0.032,and 0.046,respectively.The relative errors are 2.42%,2.76%,2.23%,and 2.43%,respectively.It is proved that the RMTS surrogate model is reliable and that the predicted data can fast provide sufficient information for the wind-resistant design of the large steerable radio telescopes.

关 键 词：METHODS NUMERICAL-METHODS data analysis-telescopes-atmospheric effects 

分 类 号：P111.44[天文地球—天文学]