Thermal Dynamic Model and Thermal Characteristics of Airships Considering Skin Transmittance

被引:0
|
作者
Cheng C. [1 ]
Wang X. [1 ]
机构
[1] School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai
关键词
Airship; Numerical calculation; Stratosphere; Thermal characteristics; Transmittance;
D O I
10.16183/j.cnki.jsjtu.2019.039
中图分类号
学科分类号
摘要
Taking stratospheric airship as the research object, considering the transmission characteristics of the airship surface and the absorption rate and emissivity of the inner filling gas to radiation, the thermodynamic equations of the airship surface skin and inner filling gas are deduced. The thermodynamic simulation model of the airship considering the transmittance of the skin is established by using the sub-method, and the thermodynamic characteristics of airship under typical skin materials are analyzed and compared. Through airship shape modeling and surface discretization, the transient thermal characteristics of each unit and internal gas are calculated, and the influence of the mesh division and time step in the simulation model on the calculation results is analyzed. The data verifies the reliability and validity of the established model and its solution method, and the thermal characteristics and the changing laws of airships with different characteristics of skin materials are analyzed and compared. © 2021, Shanghai Jiao Tong University Press. All right reserved.
引用
收藏
页码:868 / 877
页数:9
相关论文
共 21 条
  • [1] WU J T, XIA D F, WANG Z G, Et al., Thermal modeling of stratospheric airships, Progress in Aerospace Sciences, 75, pp. 26-37, (2015)
  • [2] FANG Xiande, WANG Weizhi, LI Xiaojian, A study of thermal simulation of stratospheric airships, Spacecraft Recovery & Remote Sensing, 28, 2, pp. 5-9, (2007)
  • [3] XU Xianghua, CHENG Xuetao, LIANG Xingang, Thermal analysis of a stratospheric airship, Journal of Tsinghua University (Science and Technology), 49, 11, pp. 1848-1851, (2009)
  • [4] GARDE G., Thermal modeling of NASA's super pressure pumpkin balloon, AIAA Balloon Systems Conference, (2007)
  • [5] DAI Qiumin, Study on thermal environment and thermal characteristics of airships, (2014)
  • [6] LIU Tingting, MA Zhenyu, YANG Xixiang, Et al., Influence of solar cells on thermal characteristics of stratospheric airship, Journal of Astronautics, 39, 1, pp. 35-42, (2018)
  • [7] FARLEY R., BalloonAscent: 3-D simulation tool for the ascent and float of high-altitude balloons, AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech and Balloon Systems Conferences, (2005)
  • [8] KAYHAN O, HASTAOGLU M A., Modeling of stratospheric balloon using transport phenomena and gas compress-release system, Journal of Thermophysics and Heat Transfer, 28, 3, pp. 534-541, (2014)
  • [9] YAO W, LU X C, WANG C, Et al., A heat transient model for the thermal behavior prediction of stratospheric airships, Applied Thermal Engineering, 70, 1, pp. 380-387, (2014)
  • [10] DAI Q M, XIA D F, LI X J, Et al., Performance si-mulation of high altitude scientific balloons, Advances in Space Research, 49, 6, pp. 1045-1052, (2012)