Characteristics of flow distribution of aviation kerosene in parallel pipes under supercritical pressure
|更新时间:2026-07-07
|
Characteristics of flow distribution of aviation kerosene in parallel pipes under supercritical pressure
Vol. 27, Issue 1, (2012)
作者机构:
北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室,北京,100191
作者简介:
基金信息:
DOI:
CLC:
Published:2012
稿件说明:
移动端阅览
RAN Zhen-hua, XU Guo-qiang, DENG Hong-wu, et al. Characteristics of flow distribution of aviation kerosene in parallel pipes under supercritical pressure[J]. 2012, 27(1).
DOI:
RAN Zhen-hua, XU Guo-qiang, DENG Hong-wu, et al. Characteristics of flow distribution of aviation kerosene in parallel pipes under supercritical pressure[J]. 2012, 27(1).DOI:
Characteristics of flow distribution of aviation kerosene in parallel pipes under supercritical pressure
Flow distribution characteristics of China No.3 kerosene (RP-3) in vertical parallel U-turn tubes were experimentally investigated under supercritical pressures.Based on the experimental results
the effects of temperature
pressure and asymmetrical heat flux to the flow distribution characteristics of the RP-3 were analyzed.In the experiments
the inner and outer diameters of the test tube are 1.8mm and 2.2mm respectively;the mass flow rate is maintained at 4g/s under the pressure from 3 to 5MPa
and the heat flux changes from 60 to 240kW/m2.The test results indicate that static unsteady phenomenon will be induced when fuel temperature is close to its pseudo-critical point under the lower pressure
which leads to flow imbalance and flow redistribution between the two tubes.In addition
the mass flow in the branch tube is significantly affected by the non-uniformity of heat flux
and the system stability can be improved effectively by the increase of pressure and which will inhibit the flow distribution differences in the parallel pipes.