1.
Numerical Simulation of Supersonic Axisymmetric Inlet Flow Field
超声速轴对称进气道流场的数值模拟
2.
Design and wind tunnel test of an axisymmetric inlet for ramjet engine
冲压发动机用轴对称进气道设计和试验
3.
An Investigation of Stable Operation Range in Supersonic Axisymmetric Inlet
超声速轴对称进气道稳定工作范围研究
4.
The Blowing-off of the Lip Separation of an Axisymmetric Supersonic Inlet and the Analysis of the Coherence of Dynamic Distortion of the Inlet
超音速轴对称进气道唇口分离流吹除及其动态畸变源相干分析
5.
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
6.
NONAXISYMMETRIC CASING ON AXIAL-FLOW COMPRESSORS
轴流压气机非轴对称机匣造型的研究
7.
The important thing to know that it has an axis of symmetry - the optical axis.
重点是知道主镜有一个对称轴——光轴。
8.
Investigation of the Hypersonic Axis-symmetricail Vehicle s Aerodynamic Performance and Its Flow Performance of the Whole Flow Path;
高超声速轴对称飞行器气动力特性及其全流道流动特征的研究
9.
Effects of non-axisymmetric IGV wakes on a low speed axial compressor
非轴对称导叶尾迹对低速轴流压气机的影响
10.
Study on Intension of Flammable Gas Cloud Deflagration with Axisymmetric Structure;
轴对称约束条件下可燃气云爆燃强度研究
11.
A Two-fluid Large-eddy Simulation of Axi-symmetric Sudden Expansion Dilute Gas-particle Flows
轴对称突扩稀疏气固流动的双流体大涡模拟
12.
Experimental Study on the Entrainment Characteristics of Axisymmetric Eductor by Using Wind Chamber
风室试验中轴对称排气引射-混合器的引射特性
13.
NUMERICAL INVESTIGATION ON A SUBSONIC AXIAL-FLOW COMPRESSOR ROTOR WITH THE IMPLEMENTATION OF NON-AXIASYMMETRIC HUB END WALL
亚音速轴流压气机转子非轴对称轮毂端壁的数值研究
14.
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
15.
Numerical Simulation of Axisymmetric Inlets Square Separator;
带内锥的轴对称进口方形分离器的数值研究
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.
Applications of Nilsson and Axial Relativistic Mean-field Plus Nearest-Orbit Pairing Interaction Model to Well-deformed Nuclei;
Nilsson及轴对称相对论平均场加邻近轨道对力模型对大形变核的应用
18.
The application of the theory of rotational characteristics will be useful in computation of aerodynamic force.
该方法的应用对轴对称体的气动力计算具有实际应用价值。