Numerical simulation of high-speed turbulent reacting coaxial jet flow using a structured grid

被引:0
作者
Mehta, RC [1 ]
机构
[1] Vikram Sarabhai Space Ctr, Aerodynam Div, Trivandrum 695022, Kerala, India
关键词
computational fluid dynamics; supersonic flows; turbulent reacting flows;
D O I
10.1243/0954410001531944
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Reacting flowfields are described by compressible turbulent Reynolds-averaged Navier-Stokes equations augmented with appropriate species continuity equations that provide for the convection, diffusion and production of each chemical species. The closure of the system of equations is achieved using a two-equation turbulence model. A single-step overall fast chemical reaction combustion model based on the eddy break-up concept is employed for the turbulence-chemistry interaction. A finite volume discretization is carried out in spatial coordinates to compute inviscid and viscous flux vectors. A multistage Runge-Kutta time-stepping scheme is used to obtain a steady state solution. The numerical algorithm is developed by taking into consideration the structured grid arrangement for a turbulent chemically reacting coaxial jet. The numerical scheme is shown to be computationally fast, easy to program and efficient. A supersonic diffusion flame is analysed and the results are compared with the available experimental data.
引用
收藏
页码:359 / 368
页数:10
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