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"回收/调节"方法在混合LES/RANS模拟方法中的应用
引用本文:陈逖,刘卫东,范晓樯,孙明波."回收/调节"方法在混合LES/RANS模拟方法中的应用[J].航空动力学报,2011,26(6):1215-1222.
作者姓名:陈逖  刘卫东  范晓樯  孙明波
作者单位:国防科学技术大学航天与材料工程学院,长沙,410073
基金项目:国家自然科学基金(10802096)
摘    要:采用一种混合大涡模拟/雷诺平均Navier-Stokes(LES/RANS)模拟方法结合三阶加权基本无振荡(WENO)格式对马赫数为2.88的压缩斜坡流动进行了数值模拟,并采用"回收/调节"方法生成入口湍流脉动边界条件.当采用固定入口边界条件时,湍流边界层会缺乏合理的湍流能量,使之抵抗逆压梯度的能力减弱,会严重高估分离...

关 键 词:混合大涡模拟/雷诺平均Navie-Stokes(LES/RANS)  加权基本无振荡(WENO)格式  "回收/调节"方法  入口湍流脉动边界条件  激波/湍流边界层干扰
收稿时间:7/11/2010 9:31:13 PM
修稿时间:9/14/2010 4:21:52 PM

Application of recycling/rescaling method in hybrid LES/RANS simulation method
CHEN Ti,LIU Wei-dong,FAN Xiao-qiang and SUN Ming-bo.Application of recycling/rescaling method in hybrid LES/RANS simulation method[J].Journal of Aerospace Power,2011,26(6):1215-1222.
Authors:CHEN Ti  LIU Wei-dong  FAN Xiao-qiang and SUN Ming-bo
Institution:CHEN Ti,LIU Wei-dong,FAN Xiao-qiang,SUN Ming-bo(College of Aerospace and Materials Engineering,National University of Defense Technology,Changsha 410073,China)
Abstract:A hybrid large eddy simulation/Reynolds-averaged Navier-Stokes(LES/RANS) simulation method together with the third-order weighted essentially non-oscillatory(WENO) scheme were used to compute the flow field of a Mach number is 2.88 compression ramp flow.A recycling/rescaling method was used to generate turbulent fluctuating inflow boundary conditions.When fixed inflow boundary conditions were applied,the incoming turbulent boundary layer could not resist the adverse pressure gradient due to lack of reasonab...
Keywords:hybrid large eddy simulation/Reynolds-averaged Navier-Stokes(LES/RANS)  weighted essentially non-oscillatory(WENO) scheme  recycling/rescaling method  turbulent fluctuating inflow boundary conditions  shock/turbulent boundary layer interaction  
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