艇載風壓計測量平流層大氣風場可行性分析
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中國氣象局創新發展專項“西部高海拔典型地區平流層觀測試驗”(CXFZ2022J066)項目資助


Feasibility Analysis of Measuring Stratospheric Atmospheric Wind Field by BoatBorne Anemometer
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    摘要:

    本文提出了一種基于搭載平流層飛行器對平流層大氣風場進行原位探測的探測系統,并詳細介紹了其工作原理、計算公式和風洞實驗結果。實驗室測試中,該探測系統的理論測量誤差值≤2.5 m/s。在常溫下的風洞試驗中,該系統表現出了良好的工作性能、系統穩定性和測量準確度。在和實驗室的風向、風速對比試驗中的相關性均超過了0.99,風速的平均絕對偏差為0.67 m/s,風向的絕對平均偏差為2.4°。2022年,中國氣象局氣象探測中心利用平流層超壓氣球搭載該系統在海拔19 km的平流層大氣中進行了原位探測試驗,對所搭載平臺周圍的風速和風向進行了探測,并對探測結果進行了比對分析。與平臺軌跡算法進行比對結果顯示,該系統具有較好的一致性;與NCEP_FNL再分析數據進行比對,顯示出東西向風速的相關性較好,達到了0.795,而南北風速的相關性較差,僅為0.33。試驗結果表明,在平流層飛行器上搭載該探測系統可以有效地探測平流層大氣風場,對于獲得平流層大氣環境數據集、提供大氣環境預報服務、開發平流層浮空器、監測平流層飛行器周圍的大氣環境、規劃飛行路線和區域停留等方面具有巨大的應用潛力。

    Abstract:

    The stratosphere is the layer of the atmosphere extending upwards about 50 km from the tropopause. The vertical stability of the atmosphere in the stratosphere is relatively high, and the vertical motion is relatively weak, primarily dominated by large-scale horizontal motion. Additionally, there is less dust in the stratosphere, the atmosphere is more transparent, and the content of water vapour is lower, so there are fewer phase transitions of water vapour. Moreover, given the large distance between the stratosphere and the ground, it is unaffected by complex underlying surface effects, and concurrently, there are fewer aircraft in this area, ensuring no interference by other aircraft. Precisely because of the peculiarity of the stratospheric atmospheric environment, its applications in the fields of high-resolution real-time reconnaissance and surveillance, missile early warning, navigation and positioning, rapid communication reconstruction, atmospheric environment monitoring, disaster prevention and mitigation, homeland security surveillance and defense, and anti-terrorism are considerable. This potential has attracted widespread attention globally. This paper proposes a detection system predicated on in-situ detection of stratospheric atmospheric wind field undertaken by a stratospheric aircraft, extensively introducing its working principle, computation formula, and wind tunnel test results. In the laboratory test, the theoretical measurement error value of the detection system is ≤2.5 m/s. In the wind tunnel test at room temperature, the system has illustrated exemplary working performance, system stability, and measurement accuracy. The correlation between wind direction and wind speed exceeds 0.99, the average absolute deviation of wind speed is 0.67 m/s, and the absolute average deviation of wind direction is 2.4°. In 2022, the Meteorological Observation Centre of the China Meteorological Administration equipped a stratospheric overpressure balloon to conduct an in-situ detection test in the stratosphere atmosphere at an altitude of 19 km, determining the wind speed and direction around the platform, and proceeding with a detailed analysis of the detection results. The comparison with the platform trajectory calculation results indicates that the system has good consistency; the comparison with the NCEP_FNL reanalysis data discloses a good correlation of east-west wind speed, reaching 0.795, while the correlation of north-south wind speed is relatively poor, only 0.33. The test results affirm that the detection system mounted on the stratospheric aircraft can effectively detect the stratospheric atmospheric wind field, and possesses vast application potential in areas such atmosphere environment planning, flight route planning, and regional stay.

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劉振宇,郭啟云,高濤,劉娜,楊加春.艇載風壓計測量平流層大氣風場可行性分析[J].氣象科技,2023,51(6):785~793

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  • 收稿日期:2022-09-15
  • 定稿日期:2023-09-12
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  • 在線發布日期: 2023-12-28
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