1.
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
2.
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
3.
Computer aided design of supersonic jet nozzle for jet mill
超音速气流粉碎机喷嘴计算机辅助设计
4.
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
5.
Gas-particle Two Phase Flow in Supersonic Cold Gas Dynamic Spray;
超音速冷气体动力喷涂过程中的气固两相流动
6.
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
7.
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
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.
AN EXPERIMENTAL STUDY OF HELIUM INJECTION WITH AN AERODYNAMIC RAMP INJECTOR IN SUPERSONIC FLOW
超音速空气流中气动斜坡喷嘴喷射氦的实验研究
11.
The Laval Nozzle Design and Numerical Simulation of Flow Field for A Supersonic Arc-spraying Gun
超音速电弧喷枪的拉瓦尔喷嘴设计及流场的数值模拟
12.
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
13.
A jet stream injecting a supersonic external flow is a common techniquefor the flight control of an aerospace vehicle.
将一股射流喷入超音速外流是飞行器飞行控制的常用方法。
14.
In conclusion we note the following general items concerning flow in supersonic nozzles.
最后，我们归纳几个关于超音速喷管流动的一般原则。
15.
THE EFFECT OF RATE OF EXPANSICN ON THE CONDENSATION OF SUPERSONIC WET STEAM FLOW IN A LAVAL·NOZZLE
膨胀率对拉伐尔喷管超音速湿蒸汽流动凝结过程的影响
16.
Effect of Fuel Flow Rate on Phase Structure and Microstructure of Hydroxyl Apatite Coatings Prepared by High Velocity Oxy-Fuel Spraying
燃气流量对超音速氧焰喷涂羟基磷灰石颗粒的影响
17.
Structural Design and Assist Gas Flow Analysis of Two-Laser Cutting Supersonic Nozzles
两种激光切割超音速喷嘴结构设计与辅助气体流场分析
18.
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。