本文介绍了在低速射流风洞上开展的二维喷管来流带旋涡的模拟实验。
In the paper were carried out experiments on two-dimensional nozzle flow with and without incoming swirling in a low-speed wind tunnel.
应用计算流体力学软件FLUENT,对固体火箭发动机喷管内的二维两相粘性湍流进行数值模拟。
A fully coupled two-phase viscid nozzle flow of SRM is numerically simulated with FLUENT software.
以此方法模拟了喷管和二维叶栅的多个非平衡态凝结流动,计算和试验测量的压力分布较好地吻合。
The nucleating flows in nozzles and cascades are simulated by this method and good agreement is obtained between experiment and calculation.
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