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蒙皮热辐射特性对平流层浮空器氦气温度影响

刘东旭 杨永强 吕明云 武哲

刘东旭, 杨永强, 吕明云, 等 . 蒙皮热辐射特性对平流层浮空器氦气温度影响[J]. 北京航空航天大学学报, 2010, 36(7): 836-840.
引用本文: 刘东旭, 杨永强, 吕明云, 等 . 蒙皮热辐射特性对平流层浮空器氦气温度影响[J]. 北京航空航天大学学报, 2010, 36(7): 836-840.
Liu Dongxu, Yang Yongqiang, Lü Mingyun, et al. Effect of envelop thermal radiative properties on the stratospheric super-pressure LTA vehicle helium temperature[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 836-840. (in Chinese)
Citation: Liu Dongxu, Yang Yongqiang, Lü Mingyun, et al. Effect of envelop thermal radiative properties on the stratospheric super-pressure LTA vehicle helium temperature[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 836-840. (in Chinese)

蒙皮热辐射特性对平流层浮空器氦气温度影响

详细信息
    作者简介:

    刘东旭(1985-),男,河南南阳人,博士生,liubuaa@163.com.

  • 中图分类号: V 274

Effect of envelop thermal radiative properties on the stratospheric super-pressure LTA vehicle helium temperature

  • 摘要: 分析了平流层球形超压浮空器在运行高度所受的各种环境辐射,研究浮空器处于热平衡状态时辐射传热、对流换热的作用规律,建立了浮空器的热平衡模型,分析太阳辐射、地面反照、地面辐射等环境辐照因素对浮空器全天各个时刻蒙皮材料和内部氦气平均温度影响,对比了吸收率、发射率和吸收发射比等辐射参数对浮空器热性能的影响.分析结果表明:具有低吸收发射比的蒙皮材料具有较好的热控效果;对于吸收发射比相同的蒙皮材料,具备低吸收率特性的蒙皮材料热控效果更为明显,更适用于长航时平流层超压浮空器.分析结果对浮空器蒙皮材料选择和总体设计具有指导意义.

     

  • [1] Cathey H M,Jr.The NASA super pressure balloon-a path to flight[J].Advances in Space Research.2009,44 (1): 23-38 [2] Cathey H M,Jr,Pierce D L.Duration flight of the NASA super pressure balloon .AIAA 2009-2808,2009 [3] Colozza A,Dolce J L.High-altitude,long-endurance airships for coastal surveillance .NASA/TM-2005-213427,2005 [4] Lobbia M A,Gong R H.A modular sizing model for high-altitude/long-endurance airships .AIAA 2006-821,2006 [5] Stefan K.Thermal effects on a high altitude Airship .AIAA-83-1984,1983 [6] Cathey H M.Advances in the thermal analysis of scientific balloons .AIAA-96-0695,1996 [7] Farley R E.Balloon ascent: 3-D simulation tool for the ascent and float of high altitude balloons .AIAA 2005-7412,2005 [8] 徐向华,程雪涛,梁新刚.平流层浮空器的热数值分析[J].清华大学学报:自然科学版,2009,49(11):1848-1851 Xu Xianghua,Cheng Xuetao,Liang Xingang.Thermal analysis of a stratospheric airship[J].Journal of Tsinghua University:Sci & Tech,2009,49(11):1848-1851(in Chinese) [9] Wang Y W,Yang C X.Thermal analysis of a stratopheric airship in working process .AIAA 2009-2805,2009 [10] 方贤德,王伟志,李小建.平流层飞艇热仿真初步探讨[J].航天返回与遥感,2007,28(2):5-9 Fang Xiande,Wang Weizhi,Li Xiaojian.A study of thermal simulation of stratospheric airships[J].Spacecraft Recovery & Remote Sensing,2007,28(2):5-9(in Chinese) [11] 姚伟,李勇,王文隽,等.平流层飞艇热力学模型和上升过程仿真分析[J].宇航学报,2007,28(3):603-607 Yao Wei,Li Yong,Wang Wenjun,et al.Thermodynamic model and numerical simulation of a stratospheric airship take-off process[J].Journal of Astronautics,2007,28(3):603-607(in Chinese) [12] 李德富,夏新林,杨小川.球形浮空器升空过程中的瞬态热响应[J].工程热物理学报,2009,30(1):108-110 Li Defu,Xia Xinlin,Yang Xiaochuan.Transient thermal response of spherical aerostats in rising process[J].Journal of Engineering Thermophysics,2009,30(1):108-110(in Chinese) [13] 夏新林,李德富,杨小川.平流层浮空器热特性与研究现状[J].航空学报,2009,30(4):577-583 Xia Xinlin,Li Defu,Yang Xiaochuan.Thermal characteristics of stratospheric aerostats and their research[J].Acta Aeronautica Et Astronautica Sinica,2009,30(4):577-583(in Chinese) [14] 杨世铭,陶文铨.传热学[M].北京:高等教育出版社,2006:372-377 Yang Shiming,Tao Wenquan.Heat transfer[M].Beijing: Higher Education Press,2006:372-377(in Chinese) [15] Zhai H,Euler A.Material challenges for lighter-than-air systems in high altitude applications .AIAA 2005-7488,2005 [16] Shoji Maekawa,Kouichi Shibasaki,Toyotoshi Kurose,et al.Tear propagation of a high performance airship envelope material .AIAA 2007-7829,2007 [17] Kang W G,Youngwook S,Kyeongsik W,et al.Mechanical property characterization of film-fabric laminate for stratospheric airship envelope[J].Composite Structures,2006,75(1/2/3/4):151-155
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出版历程
  • 收稿日期:  2010-01-06
  • 网络出版日期:  2010-07-30

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