Numerical simulation of three-dimensional, steady, isentropic, non-symmetricalflow in rocket nozzles is completed using a bicharacteristic method.
利用特征线方法数值模拟了双圆弧和抛物线两种特型喷管中的三维非对称定常等熵的超音速流场。
2
Results of turbulence intensity across the pressure node plane also show, the regular and symmetricalflow structures in the tube have been turned to turbulence.
径向湍流强度测量结果显示，此时管中流动已是复杂的三维结构，而非轴对称的二维结构。
3
By using the power element models established on symmetrical component decoupling - compensation theory, a network model with algorithm suitable for harmonic flow calculation is developed.