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基于长径比修正的飞艇对流换热准则关系式研究

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

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【作者】 刘泉徐庶民钟伟杨渐志刘明侯

【Author】 LIU Quan1,XU Shumin2,ZHONG Wei1,YANG Jianzhi1,LIU Minghou1(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)

【机构】 中国科学技术大学热科学和能源工程系中国科学技术大学工程与材料科学实验中心

【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%.

【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°.

【基金】 国家自然科学基金(11172296)资助
  • 【文献出处】 中国科学技术大学学报 ,Journal of University of Science and Technology of China , 编辑部邮箱 ,2013年05期
  • 【分类号】V274
  • 【被引频次】3
  • 【下载频次】136
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