thrust vectoring nozzle 轴对称矢量喷管
fluidic thrust-vectoring nozzle 射流推力矢量喷管
This article researches on mathematical model of the control mechanism of the thrust-vectoring nozzle. Some reasonable simplification methods are used to build this model because the control mechanism is very complication.
本文通过对矢量喷管控制机构运动规律的深入分析，采用合理的简化方法，对一些隐函数关系进行了显示化处理，建立了矢量喷管控制机构的运动学数学模型，该模型在计算精度和实时性上满足了控制要求。
参考来源 - 矢量喷管控制机构运动学模型建模及其与发动机综合控制研究·2,447,543篇论文数据，部分数据来源于NoteExpress
Lastly, the results of unsteady flow point out, counterflow thrust vectoring nozzle is a efficiency fluidic vectoring nozzle.
最后，非定常流的结果进一步表明，逆流喷管是一种较高效率的射流式矢量喷管。
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.
对于轴对称喷管模型主要进行了喷管的推力特性测量，对于实施矢量偏转后的喷管模型除了给出了喷管推力特性外，还给出了喷管的偏转效率。
As thrust vectoring nozzle is the feature of advanced fighters, the difficulties in implementing thrust vectoring are summarized.
矢量喷管是先进战斗机的特征，本文讨论了实现推力矢量存在的技术难点。
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