Thermal sensitivity factors analysis of stratospheric airships

被引：4
|
作者：
Cheng C. [1 ]
Wang X.-L. [1 ]
机构：
[1] School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai
来源：
Zhejiang Daxue Xuebao (Gongxue Ban)/Journal of Zhejiang University (Engineering Science) | 2020年 / 54卷 / 01期
关键词：
Airship; Sensitivity factors; Stratosphere; Thermal characteristics;
D O I：
10.3785/j.issn.1008-973X.2020.01.024
中图分类号：
学科分类号：
摘要：
A thermal characteristics model of the airship was established and the main thermal influence factors were analyzed by taking stratosphere airship as the research object. A complete thermal model of the stratospheric airship was established with the finite split method. The shape was modeled and the surface was discretized in order to make the established thermal model applicable to different types of airships. The distribution parameter method and the lumped parameter method were used to calculate the thermal characteristics of the skin cell and the internal filling gas. The reliability and effectiveness of the established model and its solution method were verified by relevant experimental data. The changes in the surface temperature of the airship and the temperature of the internal filling gas under the influence of 8 different thermal influence factors were calculated, and the qualitative and quantitative effects of each factor were analyzed. The conditions for extreme temperature of the airship skin were summarized. The effects and laws of different heat sources on the thermal characteristics of airships were compared, and a simplified part of the thermal characteristics model of airships was given. © 2020, Zhejiang University Press. All right reserved.
引用
收藏
页码：202 / 212
页数：10
相关论文
共 20 条
  • [1] Stefan K., Thermal effects on a high altitude airship, Lighter-than Air Conference, pp. 94-100, (1983)
  • [2] Fang X.-D., Wang W.-Z., Li X.-J., Preliminary discussion on thermal simulation of stratospheric airship, Space Return and Remote Sensing, 28, 2, pp. 5-9, (2007)
  • [3] Xu X.-H., Cheng X.-T., Liang X.-G., Thermal numerical analysis of stratospheric aerostats, Journal of Tsinghua University: Natural Science Edition, 49, 11, pp. 1848-1851, (2009)
  • [4] Xia X., Li D., Sun C., Et al., Transient thermal behavior of stratospheric balloons at float conditions, Advances in Space Research, 46, 9, pp. 1184-1190, (2010)
  • [5] Yao W., Lu X., Wang C., Et al., A heat transient model for the thermal behavior prediction of stratospheric airships, Applied Thermal Engineering, 70, pp. 380-387, (2014)
  • [6] Carlson L.A., Horn W.J., New thermal and trajectory model for high-altitude balloons, AIAA Paper, 20, 6, pp. 500-507, (1981)
  • [7] Farley R.E., BalloonAscent: 3-D simulation tool for the ascent and float of high-altitude balloons, AIAA 5th ATIO and 16th Lighter-Than-Air System Technology and Balloon Systems Conferences, (2005)
  • [8] Dai Q., Fang X., Li X., Et al., Performance simulation of high altitude scientific balloons, Advances in Space Research, 49, 6, pp. 1045-1052, (2012)
  • [9] Zheng W., Zhang X., Ma R., Et al., A simplified thermal model and comparison analysis for a stratospheric lighter-than-air vehicle, Journal of Heat Transfer, 140, 2, (2018)
  • [10] Garde G., Thermal modeling of NASA's super pressure pumpkin balloon, AIAA Balloon Systems Conference, (2007)
12