基于海军司烧( N-S )方程不可压缩粘滞液体和标准k-骚乱与稳定的状态和二个维的条件的假设当模特儿,模拟空气动力学在一个撤离试管在一列磁悬浮火车火车上拖在不同真空压力下面用 ANSYS/FLOTRAN 软件被做,阻塞比率,并且火车的形状出发并且跟踪。在不同真空压力下面的撤离试管磁悬浮火车火车的压力流动地在一样的阻塞比率条件下面被分析,然后比较。结果证明在试管的 1 000 Pa 的环境压力是最好完成效果空气动力学拖减小,并且在没有明显的差别空气动力学拖减小在之中不同优化头形状。总的来说,钝形状的尾巴和 0.25 的阻塞比率是更有效的为在 1 000 Pa 的试管压力拖火车的减小。
Based on the Navier-Stokes (N-S) equations of incompressible viscous fluids and the standard k-ε turbu- lence model with assumptions of steady state and two dimensional conditions, a simulation of the aerodynamic drag on a maglev train in an evacuated tube was made with ANSYS/FLOTRAN software under different vacuum pressures, blockage ratios, and shapes of train head and tail. The pressure flow fields of the evacuated tube maglev train under different vacuum pressures were analyzed, and then compared under the same blockage ratio condition. The results show that the environmental pressure of 1 000 Pa in the tube is the best to achieve the effect of aerodynamic drag reduction, and there are no obvious differences in the aerodynamic drag reduction among different streamline head shapes. Overall, the blunt-shape tail and the blockage ratio of 0.25 are more efficient for drag reduction of the train at the tube pressure of 1 000 Pa.