助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   火箭发动机 在 航空航天科学与工程 分类中 的翻译结果: 查询用时:1.882秒
图标索引 在分类学科中查询
所有学科
航空航天科学与工程
动力工程
武器工业与军事技术
燃料化工
工业通用技术及设备
自动化技术
材料科学
仪器仪表工业
力学
更多类别查询

图标索引 历史查询
 

火箭发动机     
相关语句
  rocket engine
    Studies on Theory and Strategy of Intelligent Fault Diagnosis for Liquid-Propellant Rocket Engine
    液体火箭发动机智能故障诊断理论与策略研究
短句来源
    Studies on the Method of Reliability Growth Test Evaluation for Liquid Rocket Engine
    液体火箭发动机可靠性增长试验评定方法研究
短句来源
    The Study on Reliability Growth Management for Liquid Rocket Engine
    液体火箭发动机可靠性增长管理研究
短句来源
    Theoretical, Numerical Simulation and Experimental Investigations of Combustion Instability in Liquid Rocket Engine
    液体火箭发动机燃烧稳定性理论、数值模拟和实验研究
短句来源
    Research on the Theory & Method of Trust Vector Measurement and the Automatic Test Technology in Rocket Engine Ground Test
    火箭发动机推力矢量测量理论、方法与自动测试技术研究
短句来源
更多       
  rocket motor
    Research on Working Process of the 85% H_2O_2-PE Hybrid Rocket Motor
    85%H_2O_2-PE固液火箭发动机工作过程研究
短句来源
    A Calculation Analysis for Structural Integrity and Reliability of Solid Rocket Motor Grain
    固体火箭发动机药柱结构完整性及可靠性分析
短句来源
    A CALCULATION OF DESCENT SEGMENT OF INTERNAL-BALLISTICS IN SOLID ROCKET MOTOR
    固体火箭发动机内弹道下降段的计算
短句来源
    INDUSTRIAL CT INSPECTING SYSTEM FOR SOLID ROCKET MOTOR
    固体火箭发动机工业CT探测系统
短句来源
    APPLICATION OF FINITE ELEMENT METHOD TO CALCULATING STRESS FIELD IN NOZZLE INSERT OF SOLID ROCKET MOTOR
    固体火箭发动机喷管喉衬应力场的有限元法计算
短句来源
更多       
  rocket engines
    Investigation of Intelligent Damage-Mitigating Control Methods for Reusable Liquid-Propellant Rocket Engines
    可重复使用液体火箭发动机智能减损控制方法研究
短句来源
    Integral Analysis of Nozzle Heat Transfer During the Deposition in the Solid Propellant Rocket Engines
    固体火箭发动机喷管沉积传热分析的积分方法
短句来源
    A STUDY ON STABILITY OF VARIABLE THRUST LIQUID PROPELLANT ROCKET ENGINES
    变推力液体火箭发动机稳定性研究
短句来源
    AN ANALYSIS ON POWER CYCLES OF LIQUID PROPELLANT ROCKET ENGINES
    液体火箭发动机动力循环效率的分析
短句来源
    ANALOG SIMULATION SYSTEM FOR THE OPERATION AND TRAINING OF STRATEGIC MISSILE LIQUID PROPELLANT ROCKET ENGINES
    战略导弹液体火箭发动机操作训练仿真模拟系统
短句来源
更多       
  propellant rocket engine
    A Simplified Model for the Design of Hypergolic Liquid Propellant Rocket Engine Combustors
    自燃推进剂液体火箭发动机燃烧室设计简化模型
短句来源
    Computer Calculation of the Hot Starting and Shutdown Transients of Liquid Propellant Rocket Engine
    液体火箭发动机热启动及关车过程计算机计算
短句来源
    Theoretical Calculation of the Thrust Chamber Radiation Cooling in a Liguid Propellant Rocket Engine and the Influence of Design Parameters on Equilibrium Heat Flux and Wall Temperature
    液体火箭发动机推力室辐射冷却的理论计算及主要设计参数对平衡热流强和平衡室壁温度的影响
短句来源
    Some Applications of the Numerical Computation Method to the Transient Calculation of Liquid Propellant Rocket Engine
    数值计算方法在液体推进剂火箭发动机瞬变过程计算中的若干应用
短句来源
    Calculation of Ablative Parameters And Performance Losses of Ablative Cooling Thrust Chamber for Liquid Propellant Rocket Engine
    液体火箭发动机烧蚀冷却推力室烧蚀参数及性能损失的计算
短句来源
更多       

 

查询“火箭发动机”译词为其他词的双语例句

 

查询“火箭发动机”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法,我们为您准备了出自英文原文的大量英语例句,供您参考。
  rocket engine
Specific impulse losses due to friction and dispersion in a gas-film cooled liquid rocket engine nozzle
      
The numerical results for the boundary layer in a liquid rocket engine (LRE) nozzle, where compressibility, the temperature factor, and flow acceleration are significant, are presented.
      
These conditions correspond to the use of jet engines, including a bypass turbojet gas generator, operating in steady mode, as well as a pulsed detonation rocket engine, as the high-pressure gas source.
      
This paper deals with the problems of mathematical simulation of the start-up of a liquid-propellant rocket engine (LPRE), which are associated with two-phase flows in the mixing heads (MH) of combustors and gas generators.
      
The instability of the working process in the combustion chamber of a solid-propellant rocket engine
      
更多          
  rocket motor
Numerical simulation of a liquid propellant rocket motor
      
Numerical computations have been carried out in an inert simulator of solid propellant rocket motor with the aid of a standard k-ω turbulence model.
      
Amplitude and frequency of self-oscillations in the chamber of a multimode liquid-fuel (Hydrazine) rocket motor
      
Influence of inverse flow on the operation of a hydrazine-based liquid-fuel rocket motor
      
Calculating the amplitude and frequency of thermokinetic self-oscillations in the chamber of a liquid-fuel rocket motor with the
      
更多          
  rocket engines
Such flows occur in elements of the gas-dynamic channel of turbojet engines and liquid-fuel rocket engines, ejector pumps, and other technical devices.
      
Cavitation stability characteristics of turbine-driven pump units for rocket engines
      
Heat transfer in the thrust chamber is of great importance in the design of liquid propellant rocket engines.
      
This model can be applied to all kinds of liquid propellant rocket engines as well as similar constructions.
      
Cavitation is one of the major problems in the development of rocket engines.
      
更多          
  propellant rocket engine
This paper deals with the problems of mathematical simulation of the start-up of a liquid-propellant rocket engine (LPRE), which are associated with two-phase flows in the mixing heads (MH) of combustors and gas generators.
      
The instability of the working process in the combustion chamber of a solid-propellant rocket engine
      
This work presents a numerical simulation of the flow field in a liquid propellant rocket engine chamber and exit nozzle using techniques to allow the results to be taken as starting points for designing those propulsive systems.
      
Study of working process instability in the two-chamber solid-propellant rocket engine
      
The mechanism of low-frequency acoustic instability generation in the two-chamber tandem solid-propellant rocket engine is studied numerically using the Davydov method (the method of large particles).
      
更多          
  其他


点击这里查询相关文摘
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关火箭发动机的内容
在知识搜索中查有关火箭发动机的内容
在数字搜索中查有关火箭发动机的内容
在概念知识元中查有关火箭发动机的内容
在学术趋势中查有关火箭发动机的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社