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Volume 28 Issue 6
Jun.  2002
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Journal of Beijing University of Aeronautics and Astronautics  > 2002  >  28(6): 671-674.
DONG Su-jun, LIU Meng, WANG Junet al. Simulation Study on the Thermodynamics System of Aircraft Avionics Pod[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(6): 671-674. (in Chinese)
Citation: DONG Su-jun, LIU Meng, WANG Junet al. Simulation Study on the Thermodynamics System of Aircraft Avionics Pod[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(6): 671-674. (in Chinese)
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Simulation Study on the Thermodynamics System of Aircraft Avionics Pod

  • Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 29 May 2001
  • Publish Date: 30 Jun 2002
    Abstract
  • Simulation model of the thermodynamics system of aircraft avionics pod was established and its dynamic characteristics of thermal load and main temperature parameters during the whole flying were obtained, which assisted in the selection and verification of the refrigeration system. In addition, a valid proposal about the optimization of the hull framework was offered. The study proved that dynamic simulation is an advanced calculation and analysis method for the design and model selection of the refrigeration system.

     

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  • [1] 杨方廷,张红林,赖纯洁.基于MATRIXx的引黄工程水力学仿真系统[J]. 系统仿真学报,2000,12(4):413~419. [2]丁国良,李 灏,陈江平,等. 制冷压缩机热力性能的神经网络模拟[J]. 上海交通大学学报,1999,33(3):265~267. [3]董素君,王 浚. KM6大型空间环模器氦制冷系统仿真研究[J]. 低温工程,1999,108(2):27~33.
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