Viscosity Measurement of Aviation Kerosene RP-3 Using a Double-Capillary Viscometer with Equal Mass Flow

doi:10.7652/xjtuxb201703009

您当前的位置：

首页 >

文章列表页 >

Viscosity Measurement of Aviation Kerosene RP-3 Using a Double-Capillary Viscometer with Equal Mass Flow

更新时间：2025-07-09

- Viscosity Measurement of Aviation Kerosene RP-3 Using a Double-Capillary Viscometer with Equal Mass Flow
- Vol. 51, Issue 3, Pages: 48-53(2017)
- 作者机构：
  
  西安交通大学动力工程多相流国家重点实验室,西安,710049
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb201703009
  CLC： O621.2;TK123
- Online First：10 March 2017，
  
  Published：2017
- 稿件说明：
移动端阅览
Viscosity Measurement of Aviation Kerosene RP-3 Using a Double-Capillary Viscometer with Equal Mass Flow[J]. 2017, 51(3): 48-53.
DOI：

Viscosity Measurement of Aviation Kerosene RP-3 Using a Double-Capillary Viscometer with Equal Mass Flow[J]. 2017, 51(3): 48-53. DOI： 10.7652/xjtuxb201703009.

摘要

为实现超临界压力下航空煤油RP-3的动力黏度测量

在原双毛细管黏度计对比计算法基础上

采用等流量法并引入离心力修正系数对测试段毛细管压降进行修正

测量压力可达10 MPa

测量温度范围提高至306.6～673.4 K。等流量法根据上下游毛细管质量流量相等

通过测试流体在上下游毛细管中的压降关系及下游测试段毛细管热膨胀系数推算出该流体动力黏度。该方法简便可靠

在所测温度范围内的相对标准不确定度为1.16%～2.92%。通过纯物质十二烷及质量比为1:1的正辛烷正庚烷二元混合物对等流量法进行标定

试验结果与文献值的相对偏差在±2.18%以内

相对偏差绝对平均值小于0.74%。在压力为3、4、5 MPa

温度为306.6～673.5 K的条件下

采用该方法测量了航空煤油RP-3的动力黏度。该方法的应用可为进一步提高超临界航空煤油动力黏度的测量温度范围创造条件。

Abstract

To measure the viscosity of the aviation kerosene RP-3

this paper proposed a new flow meter based on the double-capillary viscometer with the comparison calculation and the centrifugal effect due to coiling of the capillary being considered to revise the pressure drop of tested capillary. This calculation was applied to the measurement of viscosities of aviation kerosene at supercritical pressures up to 10 MPa and temperatures from 306.6 K to 673.5 K. The viscosity of the tested fluid is deduced through the measured relationship of the pressure drop between the upstream and downstream capillaries and the thermal expansion of the downstream capillary. The relative standard uncertainty of dynamic viscosity measurement is identified as 1.16%-2.92% within this paper's measuring range of temperatures. The n-dodecane and the binary mixtures of n-octane and n-heptane with a mass ratio of 1:1 were tested. The results showed a relative deviation within ±2.18% and an absolute average relative deviation below 0.74%. The viscosity of aviation kerosene RP-3 was measured on the basis of the calibration experiments at the pressures of 3

4 and 5 MPa and the temperatures from 306.6 K to 673.5 K. The method can be further extended for a larger temperature measurement range of the dynamic viscosity of aviation kerosene under supercritical pressures.

关键词

Keywords

references

FRY R S. A century of ramjet propulsion technology evolution [J]. Journal of Propulsion and Power, 2004, 20(1): 27-58.

ZHONG Fengquan, FAN Xuejun, YU Gong, et al. Heat transfer of aviation kerosene at supercritical condition [J]. Journal of Thermophysics and Heat Transfer, 2009, 23(3): 543-550.

EDWARDS T. Cracking and deposition behavior of supercritical hydrocarbon aviation fuels [J]. Combustion Science and Technology, 2006, 178(1/2/3): 307-334.

HOU Lingyu, DONG Ning, SUN Dapeng. Heat transfer and thermal cracking behavior of hydrocarbon fuel [J]. Fuel, 2013, 103: 1132-1137.

LIU Zhaohui, BI Qincheng, GUO Yong, et al. Hydraulic and thermal effects of coke deposition during pyrolysis of hydrocarbon fuel in a mini-channel [J]. Energy Fuels, 2012, 26(6): 3672-3679.

BERG R F. Quartz capillary flow meter for gases [J]. Review of Scientific Instruments, 2004, 75(3): 772-779.

BERG R F. Simple flow meter and viscometer of high accuracy for gases [J]. Metrologia, 2005, 42(1): 11-23.

MAY E F. Transport properties of argon at zero density from viscosity-ratio measurements [J]. Metrologia, 2006, 43(3): 247-258.

MAY E F, MOLDOVER M R, BERG R F, et al. Reference viscosities of H2, CH4, Ar, and Xe at low densities [J]. International Journal of Thermophysics, 2007, 28(4): 1085-1110.

ZHANG Jintao, LIN H, CHE J. Effects of connecting tubing on a two-capillary viscometer [J]. Metrologia, 2013, 50(4): 377-384.

杨竹强, 冯松, 潘辉, 等. 双毛细管式碳氢化合物黏度测量方法研 [J]. 西安交通大学学报, 2015, 49(7): 37-41.

YANG Zhuqiang, FENG Song, PAN Hui, et al. Viscosity measurement of hydrocarbons using a two-capillary viscometer [J]. Journal of Xi'an Jiaotong University, 2015, 49(7): 37-41.

YANG Zhuqiang, LIU Zhaohui, BI Qincheng, et al. Viscosity measurements of hydrocarbon fuel at temperatures from(303.2 to 513.2)K and pressures up to 5.1 MPa using a two-capillary viscometer [J]. Thermochimica Acta, 2015, 617(10): 1-7.

LIU Zhaohui, TRUSLER J P M, BI Qincheng. Viscosities of liquid cyclohexane and decane at temperatures between(303 and 598)K and pressures up to 4 MPa measured in a dual-capillary viscometer [J]. Journal of Chemical Engineering Data, 2015, 60(8): 363-2370.

KIM C S. Thermophysical properties of stainless steels [M]. Illinois, USA: Argonne National Laboratory, 1975: 1-24.

DENG H W, ZHANG C B, XV G Q, et al. Viscosity measurements of endothermic hydrocarbon fuel from(298 to 788)K under supercritical pressure conditions [J]. Journal of Chemical Engineering Data, 2012, 57(2): 358-365.

DENG Hongwu, ZHANG Chunben, XU Guoqiang, et al. Visualization experiments of a specific fuel flow through quartz-glass tubes under both sub-and supercritical conditions [J]. Chinese Journal of Aeronautics, 2012, 25(3): 372-380.

KNAPSATAD B. Viscosity of three binary hydrocarbon mixtures [J]. Journal of Chemical Engineering Data, 1991, 36: 84-88.

DYMOND J H, YOUNG K J. Transport properties of nonelectrolyte liquid mixtures: I Viscosity coefficients for n-alkane mixtures at saturation pressure from 283 to 378 K [J]. International Journal of Thermophysics, 1980, 1(4): 331-344.

CAUDWELL D R. Viscosity measurements on dense fluid mixtures [D]. London, UK: Imperial College, 2004: 25-27.

LYUSTERNIK V E, ZHDANOV A G. Physical constants and properties of substances [M]. Moscow, Russia: Standards Publishing, 1973: 214-225.

DENG H W, ZHANG C B, XV G Q, et al. Density measurements of endothermic hydrocarbon fuel at sub-and supercritical conditions [J]. Journal of Chemical Engineering Data, 2011, 56(6): 2980-2986.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Turbulent Kinetic Energy Dissipation Mechanism of Supercritical Carbon Dioxide Leakage Flow in a Scallop Bionic Seal Cavity

Bi-Level Multi-Obj ective Optimization of a Wind-Solar Coupled Hydrogen Production System Based on the Synergy of Hybrid Electrolyzer Arrays

Integrated and Joint Design Optimization of Centrifugal Compressor Impeller and Casing Treatment at Multiple Working Points

Effects of Expansion Angle Crater Film Hole on the Film Cooling Characteristics of a Double-Wall Structure

Review of the Application of EBSILON Software in Combined Heat and Power System Optimization

Related Author

No data

Related Institution

No data

⁰