nozzle axis 喷嘴轴线
omni axis nozzle 全向喷管
single axis nozzle 单轴转向喷管
axis symmetry nozzle 轴对称喷管
axis symmetrical nozzle 轴对称喷管
When the distance of two nozzles was fixed, the offset of impinging stagnation point on the axis increased with the ratio of velocity and the nozzle diameter.
当喷嘴间距一定时,轴线撞击面驻点偏移量随气速比和喷嘴直径的增大而增大。
Then, the experiment of flow separation in the nozzle was done with a solid rocket motor, and the inside pressure data along the axis of the nozzle was gotten.
然后,利用某型号固体火箭发动机进行喷管分离流试验,测得了喷管壁面上沿轴向的压强分布数据。
The flow properties including chemical species distribution along axis of the nozzle were also presented.
并给出计算条件下喷管轴线上的物理量和化学组元分布。
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