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- 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。
- 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。
- Internal performance of unsteady flow of counterflow thrust vectoring nozzle has researched base on numerical simulation. 摘要基于数值模拟方法，研究了逆流矢量喷管非定常内流性能。
- 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。
- thrust vector nozzle 推力矢量喷管
- Research of Turbofan Engine Transient Process with Thrust Vectoring Nozzle 带矢量喷管的涡扇发动机动态过程研究
- A Study on Co-Operating Between Thrust Vectoring Nozzle and Aeroengine 矢量喷管与发动机的共同工作研究
- For the jet tab TVC,the thrust and lateral forces and thrust vector deflection angles with respect to the nozzle exit area blockage ratio and the depth of water were obtained. 对扰流片推力矢量方式 ,获得了推力、侧向力、推力矢量角随发动机喷口堵塞面积比、水深的变化规律。
- By measuring the thrust and lateral forces of solid rocket motor during firing conditions,the thrust vector control performances of jet tab TVC and movable nozzle TVC were studied. 通过测量固体火箭发动机水下工作过程中的推力和侧向力,研究了扰流片和摆喷管两种推力矢量方式的水下推力矢量特性。
- thrust vectoring nozzle 矢量喷管
- fluidic thrust vectoring nozzle 射流推力矢量喷管
- The thrust vector control(TVC) performance test of solid rocket motor is presented in this paper. 本文介绍了固体火箭发动机水下推力矢量特性试验。
- The nonlinear model of a maneuverable aircraft which with thrust vector control (TVC) was established. 通过引入推力矢量技术，建立带推力矢量的飞机非线性数学模型；
- In the paper,nozzle basic concept,work theory and development of fluidic thrust vectoring techniques are introduced. 射流推力矢量控制技术是一种全新概念推力矢量技术,其具有机械式推力矢量喷管无法比拟的优点。
- The force for thrust vector control produced by the secondary injection gets bigger with the increase of flow mass and angle. 塞式喷管轴向力的增加随着二次流流量的增加而增加,但是二次流对轴向力的增加与二次流喷射的角度成反变关系。
- In two examples of half-flip and augmented circling, routine maneuver performance is calculated and the changes for thrust vector are evaluated. 以半筋斗和加力盘旋为例计算了带推力矢量作战飞机的常规机动性能，并对带推力矢量作战飞机常规机动性能的变化进行了评估。
- The Dynamic equations of a fighter with thrust vector are built, the evaluation standards of routine maneuver performance in horizontal and vertical are ascertained. 摘要建立了带推力矢量作战飞机的运动方程，确定了垂直面和水平面内常规机动性能的评估指标。
- It can be concluded that both reaction jet control system (RCS) and thrust vector control (TVC) can be used in the over the shoulder mission. The velocity loss is inevitable and the loss generated by RCS is less than that by TVC during the agile turn. 结果表明反作用喷气控制系统和推力矢量控制系统都可以用于越肩发射,在转弯过程中速度损失是不可避免的,反作用喷气控制系统可以产生的速度损失较小。
- The spherical convergent flap nozzle( SCFN) is an advanced hybrid axisymmetric/ nonaxisymmetric thrust- vectoring nozzle. 球形收敛调节片喷管(CFN)一种正在研制中的先进的轴对称/轴对称混合式推力矢量喷管。
- On the other hand, close loop model fuzzy control is studied for a classical thrust vector electrohydraulic servo control system with low damping ratio and improves dynamic performance of the system. 此外，本文根据电液位置伺服系统阻尼比低的特点，采用闭环模型模糊控制，改善了系统的动态性能。
