Deere k a . computational investigation of the aerodynamic effects on fluidic thrust vectoring . aiaa 2000 - 3598 乔渭阳,蔡元虎.基于次流喷射控制推力矢量喷管的实验及数值研究.航空动力学报, 2001 , 16 ( 3 )
The characters of the synthetic jet itself and the interaction between the two jets are the main reasons of vectoring control 其应用原理主要是由于合成射流本身所具有的特点以及其与受控流的相互祸合作用。
Identified , over “ r ” . turn left heading 130 , radar vectoring for ils approach r / w31 , standby descend , maintain fl160 已识别在r点，左转航向130度，雷达引导你盲降进入，跑道31号，等一等下降，保持高度层160 。
The thrust - vectoring nozzle control and integrated control of the engine and thrust - vectoring nozzle are researched in this paper 这样，不仅使模型完全达到实时性要求，而且使得计算过程思路更加清晰，易于理解。
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。
The application of thrust vectoring control technology makes the aircraft possess the ability to fly in post - stall domain , therefore the flight envelope is extended 推力矢量控制技术在战斗机上的应用，使战斗机有能力进入过失速飞行领域，使飞机的飞行包线得以扩展。
Especially the secondary vortex is also captured . 4 . vectoring of a primary jet with a single or two adjacent microjets in a pull mode was numerically investigated 在三维数值模拟中还捕捉到了二次涡，这为以后进一步研究微射流旋涡对的细微结构打下了良好的基础。
In order to obtain transient mathematical model as vectoring deflection which is very important in engineering and valuable in theory , three - dimensional and unsteady flow fields must be researched 由于气流在喷管流动中具有复杂的三维非定常的特征，因此，建立其动态数学模型有着更为重要的工程及理论价值。
A 3 - d viscosity turbulence model is used to analyze the unsteady around flow field of the thrust - vectoring engine of the jet vane , and results of the area including vane base , vane flake and motor shell are presented 摘要以推力矢量发动机的燃气舵为研究对象，采用三维、粘性、湍流流动模型和数值分析的接触网格技术，在定常流动计算的基础上，对包含舵基、舵片和发动机壳体的区域进行详细数值分析。
