1.
Singularity analysis of axisymmetric vectoring exhaust nozzle
轴对称推力矢量喷管运动奇异性分析
2.
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
3.
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
4.
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。
5.
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
6.
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
7.
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
8.
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
9.
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
10.
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
11.
The jet flow radiation computational method of axis-symmetry nozzle and rectangle nozzle are also discussed.
研究了轴对称喷管和二元矩形喷管喷气流辐射的计算方法。
12.
Numerical Analysis on Inner Flow Field and Thrust Speciality Research of the Asymmetry Quadrate Nozzle
非对称方形尾喷管内流场数值分析与推力特性研究
13.
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
14.
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
15.
Unsteady characteristic research of startup process of secondary hot gas injection thrust vector control system
燃气二次喷射推力矢量控制系统启动过程非定常效应研究
16.
Computational analysis on internal performance of a convergent-divergent nozzle with throat fluidic injection
带喉道注气的轴对称收扩喷管内流场计算研究
17.
And take-off kinematic equations of running take-off period of aircraft with three axes of thrust vectoring is given.
建立了带三轴推力矢量飞机的起飞滑跑段运动方程。
18.
A simulation about vector thrust control flight was completed.
针对推力矢量控制飞行进行了仿真研究。