燃气射流CFD计算软件初版本的研究

The First Version of CFD Code for Plumes

  • 摘要: 目的 发展一个燃气射流数值计算软件。方法 用时间相关法求解全NS方程及Reynolds平均应力方程,方程的时间项采用了LU分解及4步Runge-Kutta方法,对流项采用了Roe差分分裂基础上的3阶TVD级2阶、3阶ENO格式。结果与结论软件可应用于轴对称,三维燃气射流计算,格式具有高分辩和健壮稳定性,能够捕获复杂波系,计算出射流中波系与剪切层的相互作用和湍流特征。

     

    Abstract: Aim To develop CFD code for plumes. Methods Implicit LU and four step Runge Kutta were used to discretize temporal derivatives of full Navier Stokes equations and Reynolds avaraged stressed equations. The convective terms of equations were discretize by third order TVD and second and third order ENO schemes based on Roe scheme. Results and Conclusion CFD code for plumes can be used to simulate axisymmetic and three dimensional plumes. The schemes are of high resolution and robust stability, can capture complex wave structure of plumes. The interaction between wave system and shearing layer and turbulent characteristics are simulated numerically.

     

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