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1·It features embedded engines using variable area nozzles with thrust vectoring.

它采用嵌入式使用推力矢量发动机可变面积喷嘴。

2·The mathematical model of turbofan engine transient process with thrust vectoring nozzle was established.

建立带矢量喷管的涡扇发动机动态数学模型。

3·The effects of thrust vectoring angle and angular velocity of vectoring on turbofan engine operation were investigated.

研究了矢量喷管偏转角和偏转角速度对涡扇发动机工作的影响。

4·Internal performance of unsteady flow of counterflow thrust vectoring nozzle has researched base on numerical simulation.

基于数值模拟方法，研究了逆流矢量喷管非定常内流性能。

5·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。

6·The research results show that thrust vectoring technology is one of absolutely necessarily key technologies for future aircraft.

结果表明，推力矢量技术是未来战斗机必不可少的关键技术之一。

7·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。

8·The actuator at an angle can change greatly the primary jet direction and has a good effect on thrust vectoring without increasing input power.

在不增加激励器输入功率的情况下，带倾角激励器可以极大地增加主流偏转角度，推力向量控制效果很好。

9·In this paper, the flow mechanism and the applications of thrust vectoring using synthetic jet are studied in theory, numerical simulation and experiment.

本文采用理论分析、数值模拟与实验相结合的方法对合成射流流动机理及推力向量控制中的应用进行研究。

10·The thrust vectoring control technology and post-stall maneuverability enhance the aircraft's combat effectiveness greatly, and cause the worldwide interest.

推力矢量控制技术和过失速机动使战斗机的空战效能大大增加，引起了世界各国的关注。