高空科学气球下降过程航迹与热性能耦合分析

上海交通大学学报（自然版） ›› 2016, Vol. 50 ›› Issue (04): 608-612.

高空科学气球下降过程航迹与热性能耦合分析

杨希祥

(国防科学技术大学航天科学与工程学院, 长沙 410073)

收稿日期:2015-04-28 出版日期:2016-04-28 发布日期:2016-04-28
基金资助:
高分辨率对地观测系统重大专项（GFZX0X0X01）资助

Analysis of Trajectory and Thermal Performance during Descent Stage of High Altitude Scientific Balloons

YANG Xixiang

(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)

Received:2015-04-28 Online:2016-04-28 Published:2016-04-28

摘要/Abstract

摘要： 摘要：考虑高空科学气球动力学与热力学耦合关系，研究分析下降过程飞行航迹与内部氦气热性能.建立高空科学气球热模型和下降过程动力学模型，包括太阳辐射模型、红外辐射模型、对流换热模型等，仿真得到了某高空气球下降过程高度、速度等飞行航迹参数和氦气体积、温度等热性能参数，分析了参数变化规律与变化原因.研究结果表明，高空气球下降过程存在严重超热现象，超热状态变化导致下降速度变化，下降速度变化又导致超热状态改变；下降初始阶段氦气排放质量对下降速度、下降时间和超热状态均存在重要影响.

关键词: 高空科学气球, 下降过程, 航迹, 热性能

Abstract: Abstract： Considering the coupled relation between dynamics and thermodynamics, the trajectory and thermal performance of helium gas during the descent stage of high altitude scientific balloons were studied. The thermal model and vertical dynamic model of high altitude balloons were established, including the solar radiation model, the infrared radiation model, and the heat convection model. The trajectory and thermal performance of a balloon during the descent stage were simulated, including height, velocity, and volume and temperature of helium gas, while the variation regularity of parameters were analyzed. The research results show that the superheated phenomenon exits during the descent stage of balloons, state changing of superheated results in the changing of descent velocity, and changing of descent velocity results in the state changing of superheated. The discharge mass of helium gas in the initial stage has an important influence on descent velocity, descent time and superheated state. This paper can provide theoretical reference for design, flight test and application of high altitude balloons.

Key words: Key words： high altitude scientific balloon, descent stage, trajectory, thermal performance

中图分类号:

V 274

杨希祥. 高空科学气球下降过程航迹与热性能耦合分析[J]. 上海交通大学学报（自然版）, 2016, 50(04): 608-612.

YANG Xixiang. Analysis of Trajectory and Thermal Performance during Descent Stage of High Altitude Scientific Balloons[J]. Journal of Shanghai Jiaotong University, 2016, 50(04): 608-612.

参考文献

［1］HENRY M C, DEBORA A F. The 2012 NASA ~532,200 m3 super pressure balloon test flight［C］∥AIAA Balloon Systems (BAL) Conference. Florida：AIAA， 2013: 19. ［2］ANDRE V, PHILIPPE C, JACQUES M, et al. Overview of the French balloon program for the 2011 – 2012 period［C］∥AIAA Balloon Systems (BAL) Conference. Florida： AIAA， 2013: 111. ［3］KERITH F, KERIDER J F. Numerical prediction of the performance of high altitude balloons［R］. Colorado: National Center for Atmospheric Research, 1974. ［4］RODGER E F. BalloonAscent: 3D simulation tool for the ascent and floating of highaltitude balloons［R］. Maryland: NASA Goddard Space Flight Centre, 2005. ［5］DAI Qiumin,FANG Xiande, LI Xiaojian, et al. Performance simulation of high altitude scientific balloons［J］. Advances in Space Research, 2012, 49(1): 10451052. ［6］戴秋敏, 方贤德，王昊. 大气模型对高空气球运动特性和热特性的影响［J］. 计算机仿真, 2013, 30(9): 7982. DAI Qiumin, FANG Xiande, WANG Hao. Simulation of influence of different atmospheric models on dynamic and thermal properties of high altitude balloons［J］. Computer Simulation, 2013, 30(9): 7982. ［7］吕明云, 巫资春. 高空气球热力学模型与上升过程仿真分析［J］. 北京航空航天大学学报, 2011, 37(5): 505509. L Mingyun, WU Zichun. Thermodynamic model and numerical simulation of high altitude balloon ascending process［J］. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(5): 505509. ［8］姚伟, 李勇，范春石，等. 复杂热环境下平流层飞艇高空驻留热动力学特性［J］. 宇航学报, 2013, 34(10): 13091315. YAO Wei, LI Yong, FAN Chunshi, et al. Heat dynamics behavior of a stratospheric airship in a complex thermal environment at highaltitude stationkeeping conditions［J］. Journal of Aeronautics, 2013, 34(10): 13091315. ［9］赵攀峰, 李大鹏，谭百贺，等. 平流层飞艇热力学建模与仿真研究［J］. 合肥工业大学学报（自然科学版）, 2013, 36(4): 501505. ZHAO Panfeng, LI Dapeng, TAN Baihe, et al. Thermodynamic modeling and simulation of stratospheric airship ［J］. Journal of Hefei University of Technology(Science Edition), 2013, 36(4): 501505.

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