中国科学技术大学学报 ›› 2013, Vol. 43 ›› Issue (5): 387-392.DOI: 10.3969/j.issn.0253-2778.2013.05.006

• 原创论文 • 上一篇    下一篇

基于长径比修正的飞艇对流换热准则关系式研究

刘 泉   

  1. 1.中国科学技术大学热科学和能源工程系,安徽合肥 230027; 2.中国科学技术大学工程与材料科学实验中心,安徽合肥 230027
  • 收稿日期:2012-12-03 修回日期:2013-03-26 出版日期:2013-05-31 发布日期:2013-05-31
  • 通讯作者: 刘明侯
  • 作者简介:刘泉,男,1990年生,硕士生. 研究方向:平流层飞艇热控制. E-mail:lquan64@mail.ustc.edu.cn
  • 基金资助:
    国家自然科学基金(11172296)资助.

A heat transfer empirical correlation for the stratospheric airship based on its length-to-diameter ratio

LIU Quan   

  1. 1.Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei 230027, China; 2.Public Experimental Center of USTC, University of Science and Technology of China, Hefei 230027, China
  • Received:2012-12-03 Revised:2013-03-26 Online:2013-05-31 Published:2013-05-31

摘要: 飞艇热控制是平流层飞艇应用中涉及的关键技术之一,而外部对流换热是平流层飞艇热控制的重要影响因素.为了准确预测飞艇换热,基于数值模拟,建立基于飞艇长径比的对流换热准则关系式,并与实验结果比较,发现其预测误差为±7%.与0°攻角换热相比,15°攻角时迎风面换热比背风面增大了10%左右,而总体换热增大7%.

关键词: 平流层飞艇, 热控制, 热模型, 对流换热, 数值模拟, 实验研究

Abstract: Thermal control is one of the key technologies involved in stratospheric airship applications, and convective heat transfer is an important factor in the thermal control of a stratospheric airship. In order to accurately predict the heat transfer of an airship,using the numerical method, an empirical correlation of Nu number as a function of Re, Pr and l/d (length to diameter ratio) was established. Compared with experimental data, the uncertainty of the empirical correlation is about ±7%. The effect of the attack angle of an airship on heat transfer performance was evaluated. It was found that the heat transfer at the windward side is 10% higher than that of the leeward side, while the average heat transfer of airship is 7% higher when the attack angle changes from 0° to 15°.

Key words: stratospheric airship, thermal control, thermal model, convective heat transfer, numerical simulation, experimental study