中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Simulation-driven Wind Load Analysis and Prediction for Large Steerable Radio Telescopes

文献类型:期刊论文

作者Li, Shuai4; Han, Bao-Qing4; Liu, Shao-Yi4; Wang, Wen-Juan4; Wang, Ben-Ben4; Zhang, Xin-Yu4; Wang, Long-Yang4; Xu, Qian3; Wang, Na3; Zhao, Wu-Lin2
刊名RESEARCH IN ASTRONOMY AND ASTROPHYSICS
出版日期2023-02-01
卷号23期号:2页码:10
ISSN号1674-4527
关键词methods: numerical methods: data analysis telescopes atmospheric effects
DOI10.1088/1674-4527/acae6d
通讯作者Han, Bao-Qing(hanbaoqing18@163.com)
英文摘要Large steerable radio telescopes can rotate in azimuth and elevation, with various upwind postures and complex wind load characteristics. In order to (5) Corresponding authors obtain the wind load distribution on the reflector and the wind force coefficients in different upwind postures, this work took the reflector of the QiTai 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 minimum-energy 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 degrees 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.
资助项目National Key Research and Development Program of China[2021YFC2203600] ; National Natural Science Foundation of China[52275268] ; National Natural Science Foundation of China[51975447] ; National Defense Basic Scientific Research Program of China[JCKY2021210B007] ; Wuhu and Xidian University Special Fund for Industry-University-Research Cooperation[XWYCXY-012021012] ; Youth Innovation Team of Shaanxi Universities[201926]
WOS研究方向Astronomy & Astrophysics
语种英语
出版者NATL ASTRONOMICAL OBSERVATORIES, CHIN ACAD SCIENCES
WOS记录号WOS:000919891300001
资助机构National Key Research and Development Program of China ; National Natural Science Foundation of China ; National Defense Basic Scientific Research Program of China ; Wuhu and Xidian University Special Fund for Industry-University-Research Cooperation ; Youth Innovation Team of Shaanxi Universities
源URL[http://ir.xao.ac.cn/handle/45760611-7/5061]  
专题射电天文研究室_天线技术实验室
新疆天文台_110米口径全可动射电望远镜(SmART)_技术成果
脉冲星研究团组
通讯作者Han, Bao-Qing
作者单位1.Xidian Univ, Guangzhou Inst Technol, Guangzhou 510555, Peoples R China
2.China Elect Technol Grp Corp, Res Inst 39, Xian 710065, Peoples R China
3.Chinese Acad Sci, Xinjiang Astron Observ, Urumqi 830011, Peoples R China
4.Xidian Univ, Key Lab Elect Equipment Struct Design, Minist Educ, Xian 710071, Peoples R China
推荐引用方式
GB/T 7714
Li, Shuai,Han, Bao-Qing,Liu, Shao-Yi,et al. Simulation-driven Wind Load Analysis and Prediction for Large Steerable Radio Telescopes[J]. RESEARCH IN ASTRONOMY AND ASTROPHYSICS,2023,23(2):10.
APA Li, Shuai.,Han, Bao-Qing.,Liu, Shao-Yi.,Wang, Wen-Juan.,Wang, Ben-Ben.,...&Wang, Cong-Si.(2023).Simulation-driven Wind Load Analysis and Prediction for Large Steerable Radio Telescopes.RESEARCH IN ASTRONOMY AND ASTROPHYSICS,23(2),10.
MLA Li, Shuai,et al."Simulation-driven Wind Load Analysis and Prediction for Large Steerable Radio Telescopes".RESEARCH IN ASTRONOMY AND ASTROPHYSICS 23.2(2023):10.

入库方式: OAI收割

来源:新疆天文台

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