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喷流与超声速主流粘性干扰流场的数值模拟
引用本文:王江峰,伍贻兆. 喷流与超声速主流粘性干扰流场的数值模拟[J]. 南京理工大学学报(自然科学版), 2002, 26(6): 616-620
作者姓名:王江峰  伍贻兆
作者单位:南京航空航天大学航空宇航学院,南京210016;南京航空航天大学航空宇航学院,南京210016
摘    要:采用二维雷诺平均Navier-Stokes(N-S)方程时具有声速喷流的超声速主流干扰流场进行了数值求解。N-S方程的无粘项采用有限体积法在非结构网格上进行空间离散,通量分裂采用二阶精度的Vanleer格式,紊流粘性系数采用Bald-win-Lomax二层代数紊流模型计算。对当地时间步长进行了粘性修正,并发展了一种基于线化流量的逆风隐式格式以提高求解效率。

关 键 词:喷流  超音速主流  非结构网格  有限体积法  Navier-Stokes方程
修稿时间:2001-12-22

Numerical Simulation on Viscous Supersonic Crossflow with Jet Injection
WangJiangfeng WuYizhao. Numerical Simulation on Viscous Supersonic Crossflow with Jet Injection[J]. Journal of Nanjing University of Science and Technology(Nature Science), 2002, 26(6): 616-620
Authors:WangJiangfeng WuYizhao
Abstract:The numerical simulation on supersonic crossflow with jet injection was discussed. The two dimensional Reynolds averaged N-S equations were resolved on unstructured grids using finite volume method, the Vanleer fluxes vector splitting scheme was used for the non viscous terms, and the two layers Baldwin Lomax algebraic turbulent model was used for turbulent viscosity. The local time step was corrected due to the viscosity to match the convergence conditions, and an implicit scheme relying on a linearization of fluxes was developed to obtain higher convergence efficiency.
Keywords:jet   supersonic crossflow   unstructured grid   finite volume method  N-S equations
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