1.
Computation of three-dimensional flow field in secondary gas injection for thrust vectoring nozzle
气体二次喷射矢量喷管三维流场计算
2.
Heat shield position on infrared characteristics of a vectored nozzle
隔热屏位置对矢量喷管红外特征影响
3.
Singularity analysis of axisymmetric vectoring exhaust nozzle
轴对称推力矢量喷管运动奇异性分析
4.
A Method for Calculating the Effective Vectoring Angle and Flow Coefficient of an Axisymmetric Thrust-Vectoring Nozzle
轴对称矢量喷管气动矢量角和流量系数计算方法研究
5.
Characteristics of Fluidic Axisymmetric Thrust-vectoring Nozzle without Injection
轴对称射流矢量喷管非矢量状态下推力特性研究
6.
Study on the Unsteady Flow Calculation & Transient Mathematical Model of Vectoring Nozzle;
矢量喷管非定常流场计算与动态数学模型研究
7.
Design of Data Acquisition System in Aeroengine Test-run and Simulation of Vectoring Thrust Nozzle;
发动机试车台数采系统设计与矢量喷管仿真
8.
3D Computational Study of Axisymmetric Dual-throat Fluidic Thrust-vectoring Nozzles
轴对称双喉道流体控制矢量喷管三维数值模拟
9.
Flow-induced Unsteady Phenomena in Counterflow Vectoring Nozzles
逆流矢量喷管流动自身导致的非定常现象
10.
Effect of geometric parameters on performance of counterflow thrust vectoring nozzle
几何参数对逆流矢量喷管性能的影响研究
11.
Unsteady internal performance study of counterflow vectoring thrust nozzle
逆流推力矢量喷管的非定常内流性能研究
12.
Design Rules of Dual-throat Fluidic Thrust-vectoring Nozzle and Its Integration with the Afterbody of Aircraft;
双喉道射流矢量喷管的设计规律及与后机身一体化的探索
13.
Multi-objective Optimization for the Driving Mechanism of an Axial-symmetric Vectoring Exhaust Nozzle
轴对称推力矢量喷管驱动机构的多目标优化设计研究
14.
Numerical simulation on effects of flight parameters on internal flow of jet vector nozzle
飞行参数对射流矢量喷管内流场影响的数值模拟
15.
Computational investigation of slot geometric structure effects on the flow-field of shock-induced fluidic vectoring nozzle
射流缝对激波诱导矢量喷管三维流场影响的数值模拟
16.
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。
17.
A study for thrust vector control of aerospike nozzle based on second injection
塞式喷管二次喷射推力矢量控制研究
18.
Analysis of Second Gas Injection Affecting Factor on SRM Thrust Vector Control
气体二次喷射SRM推力矢量控制影响因素分析