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- The investigation shows that the separation shock wave gives an important effect on internal performance of axisymmetric vectoring nozzle. 研究结果表明，喷管内的分离激波是影响轴对称矢量喷管性能的重要因素。
- Effect of Outer Flow on Internal Performance of Axisymmetric Vectoring Nozzle 轴对称矢量喷管外流对内流干扰研究
- Performance of Mechanical Axisymmetric Vectoring Nozzle During Dynamic Deflection 机械式轴对称矢量喷管动态偏转的矢量特性研究
- Axisymmetric vectoring nozzle 轴对称矢量喷管
- Mechanism of axisymmetric vectoring exhaust nozzle(AVEN) is analyzed in the view of elastodynamic capabilities. 对轴对称矢量喷管机构进行了弹性动力学分析。
- axisymmetric vectoring exhaust nozzle 轴对称矢量喷管
- axisymmetric vectoring exhaust nozzle(AVEN) 轴对称推力矢量喷管（AVEN）
- Elastodynamic Analysis of Axisymmetric Vectoring Exhaust Nozzle 轴对称矢量喷管机构弹性动力学分析
- 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。
- 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。
- 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。
- Numerical simulation of an axisymmetric fluidic vectoring nozzle 轴对称射流矢量喷管的试验和数值模拟
- Design and Reserch of Failsafe Hydraulic System for Axisymmetric Vectoring Exhaust Nozzle 轴对称矢量喷管应急复位液压系统的设计研究
- Simulation and Reliability Analysis of Axisymmetric Vectoring Exhaust Nozzle Flexible Mechanism 矢量喷管柔性机构运动及可靠性仿真
- Experimental investigation of static internal performance for an axisymmetric vectoring thrust nozzle 轴对称矢量喷管内流特性的模型试验
- Influence of double gas flow on fluid control vectoring nozzle 双股气流对流体控制矢量喷管的影响
- The major specifications prove that the vectored nozzle control can significantly improve the flight performances at take-off when appropriately coordinated with the aerodynamic control effectors. 主要性能数据表明，矢量喷管与相应舵面协调控制明显改善了飞机的起飞性能。
- The results show that the temperature of deflected vectored nozzle varies apparently along the circumference, temperature along the deflecting direction is lower than that of the opposite direction. 结果表明：偏转矢量喷管的壁温沿周向有明显变化，沿偏转方向的壁温较低，相反方向的壁温较高。
