| 1. | Investigation of flight dynamics of thrust vectoring aircraft using extended continuation methods
应用扩展连续算法研究推力矢量飞机动力学特性 |
| 2. | 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 ) |
| 3. | 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。 |
| 4. | 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。 |
| 5. | The unsteady flow as thrust vectoring nozzle deflecting dynamically is investigated . the method of calculating the unsteady flow in the nozzle is given and the flow of the nozzle in the maximum power setting and maximum a / b power setting of the engine is calculated
研究了矢量喷管动态偏转过程中气流的非定常流动和矢量喷管非定常流动计算方法，计算了矢量喷管在发动机某中间状态和加力状态下的非定常流场。 |
| 6. | More than 200 different condition 3d viscosity steady flow fields in the thrust vectoring nozzle at different nozzle pressure ratio and different nozzle area ratio and different geometric defected angle is calculated by the program developed . and the related performance parameters are acquired by numerical simulation
利用该程序计算了某矢量喷管在不同的压比、面积比和几何偏转角下的200多种三维有粘流场，获得了矢量喷管的性能数据。 |
| 7. | Thrust vectoring is the key technique for the modem fighter with agility and post - stall maneuver ability and good flight quality . and now it is the necessary technique for the fourth generation fighter and hot technique for the performance improvement for the third generation fighter
推力矢量技术是现代战机具有敏捷性、过失速机动能力、良好的飞行品质的关键技术，其已成为第四代战斗机的必备技术和第三代战斗机改型的热门技术，得到了越来越多的重视。 |
| 8. | And establishing the model of the thrust vectoring nozzle is the base for researching thrust vectoring technique and engine performance with vectoring nozzle , especially the integration of flight and propulsion system control ( ifpsc ) . so thrust vector modeling is very important and meaningful
矢量喷管是实现推力矢量的关键部件，建立其数学模型是推力矢量技术尤其是开展带矢量喷管的发动机研究以及飞推一体化综合控制研究的基础，具有十分重要的意义。 |
| 9. | The mechanism of two possible ways of thrust vectoring control : force and moment control are analyzed . the effects of thrust vectoring on aircraft supersonic performance , take - off and landing performance , low speed and high angle of attack performance are studied . the air combat effectiveness of thrust vectoring control and post - stall maneuvers are also analyzed
5 、分析了推力矢量的两种应用方式：力控制和力矩控制的机理，研究了推力矢量对飞机超音速性能、起降性能、低速大迎角性能的影响，讨论了推力矢量与过失速机动对空战效能的影响。 |
| 10. | Cfd is also used to get the data of performance parameters of the nozzle at different nozzle pressure ratio , different nozzle area ratio and different geometric defected angle . the theory of function approximation is used to establish the transient model of thrust vectoring with the data calculated
本文通过cfd计算获得矢量喷管的性能参数，如流量系数、推力系数以及有效推力矢量角等与矢量喷管压比、面积比以及几何偏转角之间的关系数据，并利用函数逼近理论建立了矢量喷管的动态数学模型。 |
