1.
In this paper, the calculations of two-phase transonic nozzle flow are completed by a time-dependent method for the gas governing equations and by a characteristic mothod for the particle governing equations.
对气相和颗粒控制方程分别应用时间相关法和特征线法,完成了两相跨音速喷管流场的计算。
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.
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
4.
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
5.
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
6.
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
7.
trisonic aerodynamics
三音速(亚音速、跨音速 、超音速)空气动力学
8.
single subsonic jet
单亚音速喷气发动机
9.
supersonic oxygen-fuel oil burner
超音速氧-燃料油喷燃器
10.
"supersonic ""rocket"" burner"
"超音速""火箭式""喷燃器"
11.
transsuper aerodynamics
跨音速和超音速空气动力学
12.
UNSTEADY RESPONSE OF TIP LEAKAGE FLOW TO DISCRETE MICRO TIP INJECTION IN A TRANSONIC AXIAL COMPRESSOR AND ITS EFFECT ON STABILITY ENHANCEMENT
跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究
13.
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。
14.
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
15.
Study on the Microstructure and Capability of the HVOF Spraying and Designing of the Laval Nozzle;
超音速火焰喷涂陶瓷涂层的组织与性能研究及拉伐尔管的设计
16.
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。
17.
Stability of Transonic Shocks in Supersonic Flow Past a Wedge;
超音速绕流中产生的跨音速激波的稳定性研究
18.
supersonic combustion ramjet
超音速燃烧冲压喷气发动机