1.
atomized spray injectior
(喷注器) 雾化式喷嘴
2.
Investigation on spray characteristics of bi-centrifugal swirl injector
双组元离心式喷注器的喷雾特性初步研究
3.
The Effect of Oxygen Drop on Combustion Process Gas-Gas Injector
氧压降对气-气喷注器燃烧过程的影响
4.
Momentum of the injector effluent streams can contribute to lateral flow, either intentionally or unintentionally.
喷注器单元喷注射流的动量可能有意或无意地影响横向流。
5.
Resonators have been mounted on or close to the injection manifolds.
在喷注器集流腔上或其附近安装谐振器。
6.
Some stratification exists in the spray produced by any liquid propellant injector.
由任何液体推进剂喷注器所产生的喷雾都存在某些成层现象。
7.
Numerical simulation on the combustion characteristic of shear coaxial GO_2/ GCH_4 injector
气氧/甲烷同轴剪切喷注器燃烧特性数值模拟
8.
Performance comparison between the ramp injectors with different structures in supersonic combustion
不同结构超声速燃烧斜坡喷注器性能对比研究
9.
Effect of swept structure on ramp injectors in supersonic combustion
后掠结构对超声速燃烧斜坡喷注器性能的影响
10.
Study on Method in Testing Combustor Injector by Calibrating Effective Area
通过标定有效截面积检验喷注器的方法研究
11.
Also, two unique injector types, representing departures from the conventional axial injection scheme, are also discussed.
此外，还讨论了两种独特的喷注器型式，这些型式不同于常规的轴向喷射方式。
12.
The relationships between these spray parameters and the injector geometry are very complex and much still is to be learned.
这些喷雾参数和喷注器几何特性之间的关系是很复杂的，有许多问题仍需要进一步探讨。
13.
It is likely that such a coarse injector pattern would not have sufficiently high steady-state performance, and so would be unacceptable.
这样粗大的喷注器型式不会有足够高的稳态性能，因此不宜采用。
14.
The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant.
经过喷注器的压降发生变化时并不马上引起液体推进剂速度变化。
15.
Chamber compatibility and injector durability involve the control of the combustion environment.
室相容性和喷注器耐久性包括对燃烧环境的控制。
16.
aperture atomizer
喷孔式喷油嘴喷雾器
17.
a small syringe with detachable nozzles; used for vaginal lavage and enemas.
带有可分离的喷嘴的小注射器；用来洗阴道或肠。
18.
Application and Optimization of Jet Acoustic Generator in Oil Field
喷注式声波发生器在油田中的应用与优化