1.
The Design of the Fibre Winding Mold of the Solid Rocket Motor Combustion Chamber Shells
固体火箭发动机燃烧室壳体纤维缠绕模具设计
2.
Research on Heat Treatment Deformation of Big Diameter Thin Wall Combustion Chamber Case
大直径薄壁燃烧室壳体热处理变形研究
3.
Research on the Manufacturing Process of Spinning Roughcast for the Combustion Chamber Shell of a Solid Rocket Motor
固体火箭发动机燃烧室壳体旋压毛坯制造工艺技术研究
4.
housing for liquid fuel furnace burners
液体燃料燃烧器外壳
5.
Numerical Simulation of Combustion Characteristic in Combustion Chamber of SFRJ
固体燃料冲压发动机燃烧室燃烧特性数值模拟
6.
combustion efficiency
燃烧效率燃烧室效率
7.
The springs(1) are intended to hold the end cap(12) tightly seated on the asbestos washer(11) so as to seal the combustion chamber(7).
燃烧的固态燃料()一旦被导火索()燃，就在燃烧室()生大量的气体。
8.
As the fuel burns, gases expand to fill the combustion chamber at a high pressure.
当燃料燃烧时，气体膨胀，以很高的压力充满整个燃烧室。
9.
Study on the Cool Flow Field in Trapped Vortex Combustor with Air Injection
驻涡燃烧室冷态流场气体喷射的研究
10.
Model Simulation on Coupled Heat Transfer of the Components in Enging Combustion Chamber;
内燃机燃烧室部件整体耦合系统传热仿真模拟
11.
The Research on Characteristic Performance of Combustion Flow Field in Secondary Combustion Chamber for Extended Range Solid Rocket Ramjet
增程固体火箭冲压发动机补燃室燃烧特性研究
12.
Numerical Simulation Was Made of the Combusting Flow in the Gas Turbine Combustion;
燃气轮机燃烧室燃烧流场的数值模拟
13.
A chamber, such as the furnace of a steam locomotive, in which fuel is burned.
火箱，燃烧室一种燃料在里面燃烧的内室，例如蒸汽机车的燃烧室
14.
The burning of the solid fuel charge (5), once ignited by the wick (8), generates a large quantity of gas in the combustion chamber (7).
燃烧的固态燃料(5)，一旦被导火索(8)点燃，就在燃烧室(7)产生大量的气体。
15.
Research on Numerical Simulation of Two-Phase Reacting Flow Field and Combustion Performance of Annular Combustors;
环形燃烧室两相燃烧流场与燃烧性能数值研究
16.
Analysis of the combustion and flow field characteristics of advanced vortex combustor
先进旋涡燃烧室流动与燃烧特性分析
17.
Strong damping effects are possible because of solid particles in the chamber.
燃烧室内的固体颗粒可能引起强烈的阻尼效应。
18.
An Innovative Partition Model of Liquid Rocket Engine Combustion Chambers
液体火箭发动机燃烧室的一种分区模型