解茂昭

个人信息Personal Information

教授

博士生导师

硕士生导师

性别:男

毕业院校:北京航空学院

学位:硕士

所在单位:能源与动力学院

电子邮箱:xmz@dlut.edu.cn

扫描关注

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果

超临界燃料喷射过程大涡模拟:状态方程的影响

点击次数:

发表时间:2022-10-07

发表刊物:热科学与技术

所属单位:能源与动力学院

卷号:14

期号:5

页面范围:409-417

ISSN号:1671-8097

摘要:Large eddy simulations of injection and atomization of n-heptane under
   supercritical conditions were performed using commercial CFD software
   CONVERGE.The predictions were compared to experimental data provided by
   Sandia National Laboratories.Based on two cubic equations of
   state,i,e,SRK and PR equations,the effect of equations of state on
   dynamics of fuel spray,fuel jet density,the variation of mass fraction
   of fuel spray with temperature was studied and compared with
   experimental data.The simulated results show that the fuel spray
   penetration predicted by the SRK equation is deeper,and there exits a
   significant density gradient on the jet flow interface for both
   equations.The predictions agree well with the experimental results,but
   the PR equation behaves better than the SRK equation under supercritical
   conditions.The variation of mass fraction of fuel spray with temperature
   is well predicted.The sharp change in density verifies that the jet flow
   interface is a mixing layer between the liquid and its surrounding
   supercritical fluid.The density gradient can be used to identify the
   mixed layer position.

备注:新增回溯数据