coefficient of nozzle loss 喷嘴损失系数
nozzle-loss carve 嘴损曲线
nozzle loss curve 嘴损曲线
nozzle-divergence loss factor [航] 喷管扩张损失因数
relative loss of nozzle [机] 喷嘴相对损失
nozzle divergence loss factor 喷管扩张损失因数
nozzle divergent loss factor 喷管扩散损失因数
nozzle-divergent loss factor 喷管扩散损失因数
pressure loss of nozzle 水嘴压力损失
The results show that the effect of combustion efficiency on chamber pressure is limited, nozzle loss is mainly caused by its structure and size.
研究表明，补燃室压强的变化对燃烧效率的影响是有限的，喷管损失主要与喷管结构尺寸有关；
Under the same wall heat condition, with the increase of momentum correction coefficient, viscosity loss of the nozzle increases, but thrust and specific impulse decrease.
在同等壁面热条件下，随着动量调节系数的增加，喷管粘性损失增大，喷管的推力和比冲都将下降；
In the presence of the flow deflector, the generating of the vortices and the separating of the shear layer are avoided thereby the energy loss of the jet nozzle is reduced considerably.
由于喷头中有了导流体，避免了涡流的产生与剪切层的分离，从而大幅度地减少了喷头的能量损失。
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