thrust axis

基本解釋

The thrust characteristics of axis symmetry nozzle were mainly measured in test. For the nozzle having a vectoring angle, the deflection efficiency was measured too.
對于軸對稱噴管模型主要進(jìn)行了噴管的推力特性測量，對于實施矢量偏轉(zhuǎn)后的噴管模型除了給出了噴管推力特性外，還給出了噴管的偏轉(zhuǎn)效率。
Firstly, one dimensional cooling model of axisymmetric thrust chamber was formulated and empirical formulas were used. Temperature of gas wall along thrust chamber axis was obtained.
首先建立了軸對稱推力室的一維冷卻模型，并使用換熱經(jīng)驗公式，得到了推力室壁面在軸線方向上的溫度分布；
The inflectional form and the critical value's effect imposed by circumferential initial stress character on cylindrical thin shell beard the thrust at axis, accelerating upwards erect.
給出了周向初應(yīng)力數(shù)值特征對端部受推力豎直向上加速圓柱殼彈性屈曲形式和臨界力的影響。