首页 | 本学科首页   官方微博 | 高级检索  
     检索      

突然起动圆柱的非定常绕流计算
引用本文:陈则霖,杨超.突然起动圆柱的非定常绕流计算[J].空气动力学学报,1994,12(4):471-474.
作者姓名:陈则霖  杨超
作者单位:[1]北京空气动力研究所,北京100074 [2]北京航空航天大学,
摘    要:本文用分区方法定量模拟高Re数情况下突然起动圆柱的初期对称流动。绕圆柱的二维不可压流场可分为无粘区、附着粘性区和分离区。无粘区有解析解,用非定常层流边界层方程解附着粘性区,用离散涡方法处理随时间变化的分离区。试用了混合的Rankine和Lamb涡模型及二次离散涡。给出了Re=300、9500两个算例,基本符合有关实验结果。

关 键 词:空气动力  边界层  非定常流动  圆柱  绕流

Caculation of Unsteady Flows past an Impulsively Started Cylinder
Chen Zelin.Caculation of Unsteady Flows past an Impulsively Started Cylinder[J].Acta Aerodynamica Sinica,1994,12(4):471-474.
Authors:Chen Zelin
Institution:Chen Zelin(Beijing Institute of Aerodynamics)Yang Chao(Beijing University of Aeronautics and Astronautics)
Abstract:The initia1 symmetric flows around an impulsively started circular cylinder are simulated bv the zonal method in this paper.The two-dimensional imcompressible unsteady flow around cylinder is divided into inviscid,attached viscotis and separated zones.There is analytic sol-ution in the inviscid zone. The unsteady laminar boundary laycr equations are solved bV difference scheme in the attached viscous zone. The sepa-rated zone,varing with time,can be coped with discrete vortex method.The Rankine and Lamb vortex corc models are mixed,and the secondary dis-crete vortices are taken. The rcsults of sample at Re=3000, 9500 agree with available experiment.
Keywords:zonal method vortex method  circular cylinder  unsteady flow  boundary layer    
本文献已被 CNKI 维普 等数据库收录!
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