1.
Numerical study of linear periodic form HYLTE nozzle's flowfield
线性周期阵列高超音速低温喷管流场数值分析
2.
SPH simulation on agglomerate Fe particle deposition in low temperature high velocity air fuel spraying process
低温超音速喷涂团聚铁粒子沉积的SPH模拟
3.
High temperature instantaneous supersonic flow measurement using hydroxyl tagging velocimetry
高温瞬态超音速喷流OH分子示踪速度测量
4.
Microstructure and Phase Composition of Ti-Ni Coating Prepared by Low-Temperature High Velocity Oxygen Fuel Spraying and of the Same Coating After Laser Treatment
Ti-Ni低温超音速火焰喷涂层及激光处理后的特征
5.
Study on Gas Separation Performance of Vortex Tube with Supersonic Inlet Nozzles
超音速喷嘴涡流管气体分离性能研究
6.
hypersonic ramjet engine
高超音速冲击式空气喷气发动机
7.
At high speed and hot exhaust flow conditions, a preliminary experimental investigation on the divergent wall cooling of Two Dimensional C-D Nozzle had been conducted.
在高速热喷流条件下，对二元收扩喷管超音段壁面的冷却进行了初步试验研究。
8.
supersonic oxygen-fuel oil burner
超音速氧-燃料油喷燃器
9.
"supersonic ""rocket"" burner"
"超音速""火箭式""喷燃器"
10.
Microstructures and High Temperature Erosion Properties of Supersonic Arc-sprayed Composite Coatings of Cored Wires Containing Intermetallics and Nanosized Ceramics under Nitrogen Protective Atmosphere;
N_2保护超音速电弧喷涂金属间化合物纳米复合涂层的组织结构及高温冲蚀性能
11.
Research on Designing of Laval Nozzle and Characteristics of Phase Transition for Supersonic Swirling Separator;
超音速旋流分离器喷管设计与相变特性研究
12.
Numerical Simulations of Flows in the Hartmann Resonance Tube and Ultra-Sonic Gas Atomization Nozzle;
Hartmann共振管及超音速气体雾化喷嘴流场数值模拟
13.
The numerical simulating of the supersonic gas-particle two phase flow in De-Laval-Nozzle;
冷气体动力喷涂喷管内超音速气固两相流动数值模拟
14.
Investigation on Design of Altitude Control System of the Missile with Supersonic Speed at Minimum Altitude;
超音速超低空导弹高度控制系统设计与研究
15.
metal sealed UHF and low noise silicon transistor
金属壳超高频低噪音硅晶体管
16.
portable ultra-high-speed water spray system
手提式超高速喷水系统
17.
Mach Number Seven and Eight Nozzle Design of the Diameter One Meter Hypersonic Wind Tunnel and Flow Field Testing;
Φ1米高超声速风洞M7、8喷管设计及流场校测
18.
Numerical analysis of water phase transition effects in hypersonic nozzles
高超声速喷管中水蒸气凝结的数值研究