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   固体火箭发动机 在 航空航天科学与工程 分类中 的翻译结果: 查询用时:0.056秒
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固体火箭发动机     
相关语句
  solid rocket motor
    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
    Impulse Efficiency of a Solid Rocket Motor for Lateral Maneuver Control
    横向机动控制固体火箭发动机的冲量效率(英文)
短句来源
更多       
  solid rocket engine
    Heat Transfer Analysis in the Nozzle Throat Deposit Process of the Solid Rocket Engine
    (一)固体火箭发动机喷管喉部沉积过程的传热分析
短句来源
    TRANSIENT BURNING PROCESSES IN SOLID ROCKET ENGINE——FLAME-OUT PEFORMANCES AND EXPERIMENTS
    固体火箭发动机瞬态燃烧过程——熄火特性与实验
短句来源
    ESTIMATION OF UNCERTAINTY ON THRUST MEASURMENT IN 0.5%HIGH-ACCURACY MEASURING SYSTEM OF SOLID ROCKET ENGINE
    固体火箭发动机0.5%高精度测试系统推力参数测量不确定度的评定
短句来源
    PREDICTION OF COMBUSTION INSTABILITY IN SOLID ROCkET ENGINE
    固体火箭发动机燃烧不稳定性预估
短句来源
    RELIABILITY DESIGN OF CYLINDRICAL CASE OF SOLID ROCKET ENGINE
    固体火箭发动机圆柱壳体的可靠性设计
短句来源
更多       
  solid propellant rocket engine
    INVESTIGATION ON THE DECREASE OF AVERAGE PRESSURE UNDER UNSTABLE COMBUSTION IN SOLID PROPELLANT ROCKET ENGINE
    固体火箭发动机不稳定燃烧时平均压力下降的原因探索
短句来源
    Numerical Computation of Stratified Flow Field in Combustion Chamber of Solid propellant Rocket Engine
    固体火箭发动机燃烧室层流流场的数值模拟
短句来源
    Solid Propellant Rocket Engine Modal Test and Analysis Technique
    固体火箭发动机试验模态分析技术研究
短句来源
    A Study on Measurement Method of Exhaust Flames Temperature for Solid Propellant Rocket Engine
    固体火箭发动机羽焰测温方法研究
短句来源
    RESEARCH ON THE DATA PROCESSING METHOD OF SOLID PROPELLANT ROCKET ENGINE PLUME TEMPERATURE
    一种测量固体火箭发动机羽焰温度的数据处理方法研究
短句来源
更多       
  solid propellant rocket motor
    The Numerical Simulation of 3-D Flow in the Chamber of Solid Propellant Rocket Motor
    固体火箭发动机燃烧室3维紊流数值模拟
短句来源
    SOFTWARE MODEL AND THE REALIZATION OF AUTOMATIC PARAMETER DESIGN OF A SOLID PROPELLANT ROCKET MOTOR
    固体火箭发动机自动化参数设计软件模型与实现
短句来源
    Contour design and numerical calculation of certain solid propellant rocket motor nozzle
    某型号固体火箭发动机喷管型面设计与数值计算
短句来源
    STUDY ON ALGORITHMS FOR PREDICTION OF SOLID PROPELLANT ROCKET MOTOR PERFORMANCE
    固体火箭发动机内弹道性能预估方法的研究
短句来源
    THE ADVANCE AND PROSPECT ON GAS DYNAMICS OF SOLID PROPELLANT ROCKET MOTOR
    固体火箭发动机气体动力学发展的现状和方向
短句来源
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  solid rocket motor
The impact of using porous wall materials in cold flow solid rocket motor testing is addressed.
      
Particle-image velocimetry measurement in the exhaust of a solid rocket motor
      
Successful particle-image velocimetry (PIV) measurements have been demonstrated in the exhaust plume of a small solid rocket motor.
      
The interaction of solid rocket motor exhaust and deluge water released on the pad at the time of launch results in the formation of an exhaust cloud.
      
The impactor population also is separated in terms of nature of the projectiles, with most of the low-medium velocity ones being particles related to solid rocket motor slag condensates.
      
更多          
  solid rocket engine
The spectral radiant characteristics of plume particles of a solid rocket engine are important in the design of the engine specific impulse, ablative material, and plume flame hiding.
      
  solid propellant rocket engine
Following this experience, a new type of six-target eight-wavelength pyrometer for solid propellant rocket engine plume temperature distribution measurements has been developed.
      
  solid 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.
      
These methods are applied in viscous two-phase flow calculation of rocket nozzle and in the prediction of thrust and specific impulse for solid propellant rocket motor.
      
A solid propellant rocket motor can be considered to be made of various circumferential layers of different properties.
      
Application of the finite element computer program in the analysis of fracture in solid propellant rocket motor cartridge or grain is included.
      
A solid propellant rocket motor combines both the combustion chamber and the propellant storage facilities in one unit.
      
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