| 引用本文: | 杨希祥,侯中喜,麻震宇.平流层长航时气球上升过程超冷现象影响因素分析.[J].国防科技大学学报,2015,37(5):91-96.[点击复制] |
| YANG Xixiang,HOU Zhongxi,MA Zhenyu.Analysis of influential factors to supercooling phenomenon during ascent stage of stratospheric long duration balloons[J].Journal of National University of Defense Technology,2015,37(5):91-96[点击复制] |
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| 平流层长航时气球上升过程超冷现象影响因素分析 |
| 杨希祥, 侯中喜, 麻震宇 |
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(国防科技大学 航天科学与工程学院， 湖南 长沙 410073)
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| 摘要: |
| 平流层长航时气球超冷现象是指内部浮升气体温度低于外界大气温度，超冷会引起浮力损失进而阻碍气球上升过程。建立了长航时气球辐射、对流等热模型和上升过程动力学模型，仿真分析了初始净浮力、蒙皮热物性参数、放飞时间和放飞日期等因素对超冷现象的影响规律。研究结果表明，上升过程内外温差随初始净浮力增大而增大且变化显著，可见光吸收率和红外吸收率增大时，内外温差值总体上呈减小趋势；放飞时刻和放飞日期对超冷现象影响较小，但放飞时间不同，气球上升至设计驻空高度的时间差别较大。该结论可为平流层浮空器总体方案设计和放飞试验提供有益参考。 |
| 关键词: 平流层长航时气球 上升过程 超冷现象 热模型 |
| DOI：10.11887/j.cn.201505014 |
| 投稿日期：2015-01-20 |
| 基金项目:高分辨率对地观测系统重大专项资助项目（GFZX040201） |
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| Analysis of influential factors to supercooling phenomenon during ascent stage of stratospheric long duration balloons |
| YANG Xixiang, HOU Zhongxi, MA Zhenyu |
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(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)
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| Abstract: |
| Supercooling phenomenon of stratospheric long duration balloons means that the temperature of helium gas inside is lower than that of atmosphere outside, this will cause the loss of buoyancy and affect ascent process of the balloon as a result. Radiation and convection thermal models and the vertical dynamic model of long duration balloons were established, and the influence regularity of some important factors, including initial net buoyancy, skin thermal physical parameters, launch time and launch date, on supercooling phenomenon was analyzed. Simulation results show that the temperature difference between helium gas and outside atmosphere enlarges remarkably along with the increase of initial net buoyancy, and the temperature difference decreases when the absorptivity for visible light and infrared radiation increases. Simulation results also show that the influence of launch time and launch date on supercooling phenomenon is much smaller, while flight time from ground to designed altitude displays great difference when the launch time is different. The research results can provide theoretical reference for conceptual design and flight test. |
| Keywords: stratospheric long duration balloon ascent stage supercooling phenomenon thermal model |
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