摘要
用可压方法及预处理方法求解了低马赫数紊流流动,其中空间离散格式采用了Roe格式,紊流模型采用了DES模型。以绕NACA0012的紊流流动为例,分析了该方法对提高流动速度和精度的特性,并将其用到多段翼型及绕圆柱的非定常流动中。数值模拟结果表明,该方法能有效求解低速流动及混合流场问题,且具有较高的数值精度。
The preconditioning method is used to solve the low Mach number flow. The space discritisation scheme is the Roe scheme and the DES turbulence model is used. Then, the low Mach number turbulence flow around the NACA0012 airfoil is used to verify the efficiency of the proposed method. Two cases of the low Mach number flows around the multi-element airfoil and the circular cylinder are also used to test the proposed method. Numerical results show that the methods combined the preconditioning method and compressible Navier-Stokes equations are efficient to solve low Mach number flows.
