1.
Design of three dimensional afterbody/nozzle configuration of airbreathing hypersonic vehicle
高超声速飞行器后体喷管三维构型设计
2.
Ablation of nozzle convergent section insulation of solid rocket motors with long aft-finocyl grain
大后翼装药固体发动机喷管收敛段绝热层烧蚀
3.
lance for liquid- or powder-spraying machines
液体或粉末喷雾机器的喷管
4.
Computation of three-dimensional flow field in secondary gas injection for thrust vectoring nozzle
气体二次喷射矢量喷管三维流场计算
5.
Design Rules of Dual-throat Fluidic Thrust-vectoring Nozzle and Its Integration with the Afterbody of Aircraft;
双喉道射流矢量喷管的设计规律及与后机身一体化的探索
6.
3D afterbody nozzle optimization of air-breathing hypersonic vehicle
吸气式高超声速飞行器三维后体尾喷管优化设计
7.
STUDY ON LIQUID ADDITION UNDER VACUUM POST PELLETING OF FEED;
颗粒饲料液体真空后喷涂工艺的研究
8.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的
9.
The reclamation nozzle captures a portion of the spent driver gas.
回收喷管收集一部分用过的驱动气体。
10.
Study on the Hydrodynamics Behavior of Spout-fluid Bed with a Draft Tube;
导向管喷动流化床流体力学特性研究
11.
The Development of Integral Design of Solid Rocket Motor Nozzle;
固体火箭发动机喷管热结构CAD设计
12.
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
13.
Micronozzle flow based on simulation of molecule movement
基于分子运动模拟的微喷管流体流动
14.
Numerical investigation on gas flow in Laval micronozzle
Laval型微喷管内气体流动的计算及分析
15.
The Study on Hydrodynamics and Desulfurization Characteristics in Duble Nozzles Rectangular Draft Tube Spouted Bed;
双喷嘴矩形导流管喷动床流体力学特性及脱硫性能的研究
16.
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
17.
Analysis of Interior Ballistics of Reduced Recoil Structure with Front Nozzle
喷管前置式减后坐武器内弹道机理分析
18.
In order that thermal sprayed coats are made to have higher adhesive strength,commonly a thin layer of bonding is precoated,then the functional layer is sprayed again.
为了使热喷涂层有高的结合强度，一般要在基体上先喷一薄的底层，然后再喷工作层。