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高空气球热力学模型与上升过程仿真分析
引用本文: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.
作者姓名:吕明云  巫资春
作者单位:北京航空航天大学 航空科学与工程学院, 北京 100191
摘    要:基于对高空气球热力学环境的分析,建立了热力学与动力学耦合的高空气球动力学模型;并采用该模型对某高空气球的上升与驻留过程进行仿真分析.结果表明:高空气球上升过程中内部氦气存在"超冷"现象,其中平流层区域"超冷"明显,氦气平均温差为-19 K;由于"超冷",其上升速度曲线呈双"V"形变化;强太阳辐射与弱对流环境使驻留过程中氦气呈现"超热"现象,平衡时氦气平均温度比环境温度高39 K,球内氦气超压648.8 Pa.数值仿真的速度、平均温度变化规律与相关飞行试验数据相吻合,说明该仿真模型是有效的. 

关 键 词:高空气球    热力学模型    热辐射    动力学模型    数值仿真
收稿时间:2010-03-05

Thermodynamic model and numerical simulation of high altitude balloon ascending process
Lü 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.
Authors:Lü Mingyun  Wu Zichun
Institution:School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:Based on the analysis of the high-altitude balloon thermodynamic environment,a coupling dynamic model was established to describe its thermodynamics and kinetics.The model was used to simulate the ascending and floating processes of a high altitude balloon.The results show that the inner helium temperature will present supercool during its ascending process,and supercool is more pronounced during the stratosphere region,with the inner helium temperature 19K below the surrounding air temperature.Because of s...
Keywords:high altitude balloon  thermodynamic model  thermal radiation  dynamic model  numerical simulation  
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