超声速平板边界层旁路转捩直接数值模拟

Direct numerical simulation of by-pass transition of the supersonic flat plate turbulent boundary layer

  • 摘要: 采用具有七阶精度的有限差分格式和基于Euler方程组的特征边界条件, 通过直接数值模拟研究了由固定相位周期性吹吸扰动诱导的、Ma=2.25、Re=2.5×107/m(635 000/inch)空间发展平板边界层的旁路转捩过程, 并建立了相应的直接数值模拟数据库。数值结果表明:扰动相位的随机性并不是转捩发生的必要条件, 固定相位周期性吹吸扰动即可诱发边界层的转捩;当采用固定相位时, 随着吹吸频率的增加, 转捩位置向下游移动;当扰动频率足够大时, 周期性吹吸无法诱导出边界层的转捩。随后, 在所得数据库中提取了速度及热力学变量的平均值, 与已有的数据库和理论分析吻合良好;速度脉动均方根与公认的不可压缩平板边界层实验基本吻合;热力学变量脉动均方根和雷诺应力与已有数据库的统计结果及实验数据具有相同的分布特征。对比发现, 不同转捩的诱导因素对平均转捩位置和热力学变量均方根、雷诺应力等高阶统计量的影响较大。

     

    Abstract: Using the characteristic boundary conditions and high-order finite difference schemes, direct numerical simulation(DNS) was performed to investigate the effect of phase and frequency of the periodic blow and suction disturbance which was used to trigger the by-pass transition of the flat plate boundary layer with free stream Ma=2.25, Re=2.5×107/m (635 000/inch). The numerical results show that the randomness of the disturbance phase is not the necessary condition to trigger the transition, and with the deterministic disturbance phase, the average location of transition moves backward when the disturbance frequency increases. However, if the frequency is bigger than a critical value, the transition in the boundary layer will not happen. A DNS database was established under the condition of deterministic disturbance phase. The Van Direst velocity agrees well with the wall and logarithm law of incompressible flat plate boundary layer, and the turbulence intensities coincide with the incompressible flat plate experimental datum.The averaged thermodynamic variables are very close to that of reference results. These verify the present DNS results. Then, the statistics of thermodynamic variables fluctuation and Reynolds stress are extracted from the DNS database. Compared with the relative references' DNS results, the disturbance, boundary conditions and numerical methods have observably effect on the second order statistics and the averaged transition position.

     

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