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本文用一维两相喷管流动程序对几何相似的发动机(用同一种推进剂)进行了计算,得出了发动机尺寸越大,两相流损失越小的结论。
In this paper, a one-dimensional two-phase nozzle flow program for the geometry similar to the engine (using the same propellant) was calculated, the larger the engine size, the smaller the loss of two-phase flow conclusion.