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Publishing Language: Chinese

Spatiotemporal distribution characteristics of high-altitude wind shear

Junfeng YANG1,2Xuan CHENG3Jianmei WANG1,2Yiming ZHANG1,2Xiong HU1,2Cunying XIAO4,5( )
Key Laboratory of Solar Activity and Space Weather,National Space Science Center,Chinese Academy of SciencesBeijing 100190China
Key Laboratory of Science and Technology on Environmental Space Situation Awareness,National Space Science Center,Chinese Academy of SciencesBeijing 100190China
Deep Space Exploration LaboratoryBeijing 100041China
Institute for Frontiers in Astronomy and Astrophysics,Beijing Normal UniversityBeijing 100875China
Department of Astronomy,Beijing Normal UniversityBeijing 100875China
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Abstract

The vehicles at the rising stage are susceptible to being influenced by upper atmospheric wind. The high-altitude wind shear is essential in the rocket design. The synthetical wind vector approach is used to determine the wind shear features from the ground to 30 km in the East Asia region, based on the National Centers for Environment Prediction (NCEP)reanalysis data from 2020 to 2022. The findings indicate a relationship between season, altitude, and horizontal distribution and the maximum wind direction, maximum wind speed, and wind shear. The wind shear from radiosonde observations is used to analyze the difference between true atmospheric wind shear and that from NCEP. NCEP underestimates the wind shear. The attack angles of two simulated launch vehicles in the atmosphere wind are analyzed. The results indicate that wind shear has a significant impact below 5 km and between 7~18 km. These results are helpful to grasp the distribution characteristics of high-altitude wind shear in China and provide a reference for the accurate and safe rocket design.

CLC number: V411.8 Document code: A Article ID: 1001-5965(2026)01-0192-11

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Journal of Beijing University of Aeronautics and Astronautics
Pages 192-202

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Cite this article:
YANG J, CHENG X, WANG J, et al. Spatiotemporal distribution characteristics of high-altitude wind shear. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(1): 192-202. https://doi.org/10.13700/j.bh.1001-5965.2023.0738

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Received: 09 November 2023
Published: 02 February 2024
© Journal of Beijing University of Aeronautics and Astronautics