首页 | 本学科首页   官方微博 | 高级检索  
     

均匀磁场中高超声速弱电离气体流动数值模拟
引用本文:黄富来,黄护林. 均匀磁场中高超声速弱电离气体流动数值模拟[J]. 航空动力学报, 2009, 24(11): 2443-2451
作者姓名:黄富来  黄护林
作者单位:南京航空航天大学,高新技术研究院,南京,210016;南京航空航天大学,高新技术研究院,南京,210016
摘    要:采用7组元化学模型并应用组分公式计算电导率,通过求解黏性MHD(magneto-hydro-dy-namics)方程组,研究了不同强度均匀磁场对三维钝头体高超声速绕流化学非平衡流动的影响.结果表明,随着磁场的增强,激波脱体距离逐渐增加;总阻力系数和壁面温度逐渐减小.在By=0.03 T磁场作用下,与无磁场的结果相比,化学非平衡流中的激波脱体距离增加约7%,总阻力系数减小约5%,局部壁面温度最大降低74%;而冻结流中的激波脱体距离增加约43%,总阻力系数减小约6.9%,局部壁面温度最大降低18%. 

关 键 词:均匀磁场  高超声速  化学非平衡  电导率  总阻力系数
收稿时间:2008-11-10
修稿时间:2009-02-17

Numerical simulation of weakly ionized gas hypersonic flow under uniform magnetic field
HUANG Fu-lai and HUANG Hu-lin. Numerical simulation of weakly ionized gas hypersonic flow under uniform magnetic field[J]. Journal of Aerospace Power, 2009, 24(11): 2443-2451
Authors:HUANG Fu-lai and HUANG Hu-lin
Affiliation:Academy of Frontier Science, Nanjing university of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Seven-species air model was used and electrical conductivity was calculated by species formula to investigate the effects of the intensity of uniform magnetic field on three dimensional chemical nonequilibrium hypersonic flows around a blunt body by solving the viscous MHD(magneto-hydro-dynamics) equations.The results show that the shock standoff distance is increased and total drag coefficient and wall temperature are reduced with increasing external magnetic field.At By=0.03 T,the shock standoff distance is increased by about 7%,total drag coefficient and local wall temperature in nonequilibrium flow are decreased by about 5% and 74%,respectively.However,in frozen flow under the same conditions,the shock standoff distance is increased by about 43%,total drag coefficient and local wall temperature are decreased by about 6.9% and 18%,respectively,as compared with that without magnetic field.
Keywords:uniform magnetic field  hypersonic  chemical nonequilibrium  electrical conductivity  total drag coefficient
本文献已被 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号