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亚临界压力下航空煤油RP-3动力黏度测量

贾洲侠 徐国强 邓宏武 闻洁

贾洲侠, 徐国强, 邓宏武, 等 . 亚临界压力下航空煤油RP-3动力黏度测量[J]. 北京航空航天大学学报, 2014, 40(7): 934-938. doi: 10.13700/j.bh.1001-5965.2013.0456
引用本文: 贾洲侠, 徐国强, 邓宏武, 等 . 亚临界压力下航空煤油RP-3动力黏度测量[J]. 北京航空航天大学学报, 2014, 40(7): 934-938. doi: 10.13700/j.bh.1001-5965.2013.0456
Jia Zhouxia, Xu Guoqiang, Deng Hongwu, et al. Dynamic viscosity measurements of aviation hydrocarbon fuel RP-3 at sub-critical pressures[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(7): 934-938. doi: 10.13700/j.bh.1001-5965.2013.0456(in Chinese)
Citation: Jia Zhouxia, Xu Guoqiang, Deng Hongwu, et al. Dynamic viscosity measurements of aviation hydrocarbon fuel RP-3 at sub-critical pressures[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(7): 934-938. doi: 10.13700/j.bh.1001-5965.2013.0456(in Chinese)

亚临界压力下航空煤油RP-3动力黏度测量

doi: 10.13700/j.bh.1001-5965.2013.0456
基金项目: 

国家自然科学基金资助项目(50676005)

详细信息
    作者简介:

    贾洲侠(1987-),男,山西太原人,博士生,zxjia914@163.com.

  • 中图分类号: V312

Dynamic viscosity measurements of aviation hydrocarbon fuel RP-3 at sub-critical pressures

  • 摘要: 基于经典的毛细管测量流体黏度原理,提出一种新型的测量高温高压条件下的单相介质流体黏度的方法及实验设备.经过误差分析,该方法具有1.009%的测试误差.利用该方法对蒸馏水的动力黏度(2 MPa,295~400 K)进行了标定实验,实验结果表明动力黏度测量的平均偏差小于0.715%,其最大偏差不超过2.3%.然后对国产航空煤油RP-3在压力0.1~2 MPa下,温度为298~744 K下动力黏度进行了测量.该方法适用于均一的牛顿流体.

     

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  • 被引次数: 0
出版历程
  • 收稿日期:  2013-08-01
  • 网络出版日期:  2014-07-20

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