Input is simply a list of propellant ingredients, as well as chamber pressure and nozzle exit pressure.
投入，简直是名单推进剂成分，以及商会的压力和喷嘴出口的压力。
Eventually we will have lowered the back pressure enough so that it is now equal to the pressure at the nozzle exit.
最终我们将有降低回压足以使现在是相等的压力，在喷嘴出口。
The discrete vortex method was adopted to simulate and analyze the vortex structure and pressure distribution of the flow field at the nozzle exit.
采用离散涡方法模拟了两种不同形状哨嘴的喷嘴出口流场旋涡结构和压力分布。
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