固体火箭冲压发动机,solid rocket ramjet
1)solid rocket ramjet固体火箭冲压发动机
1.Quick-forecasting algorithm for performance ofsolid rocket ramjet;固体火箭冲压发动机性能快速预估算法
2.Some technological problems ofsolid rocket ramjet;固体火箭冲压发动机的若干技术问题
3.Experimental study onsolid rocket ramjet with central air-inlet mode;中心进气式固体火箭冲压发动机试验研究
英文短句/例句
1.An Application Research of Integral Sol id Propellant Rocket Ramjets整体式固体火箭冲压发动机的应用性能探讨
2.The Solid Rocket-Ramjet Engine Thrust Calculation and Experimental Research of Connected-Pipe Testing;固体火箭冲压发动机推力计算与实验研究
3.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
4.Predominance of Ducted Solid Rocket Ramjet Applied to Airborne Missile固体火箭冲压发动机在空空导弹上应用的优势
5.Research on Thermal Protecting of Afterburning Chamber for Integral Solid Rocket-ramjet固体火箭冲压发动机补燃室梯度热防护体系研究
6.Research on the Secondary Combustion Chamber Operation Process of Boron-Based Propellant Ducted Rockets;含硼推进剂固体火箭冲压发动机补燃室工作过程研究
7.Three-Dimensional Numerical Simulation of Afterburner Flow Field of Solid Rocket Ramjet固体火箭冲压发动机补燃室流场三维数值计算研究
8.Study on theoretical performance of solid ducted rocket based on thermodynamic calculation基于热力计算的固体火箭冲压发动机理论性能研究
9.Effects of Jet Rotational Angle on the Second Combustor of Boron-based Propellant Solid Rocket Ramjets含硼固体火箭冲压发动机中燃气旋流角对补燃室的影响
10.Aerodynamic Design of Turbo for Solid Rocket Turbo Ramjet Engine;固体火箭涡轮冲压发动机涡轮气动设计
11.turbo-ram rocket engine涡轮冲压式火箭发动机
12.Characteristics tests of pulse liquid rocket engine with high chamber pressure高室压脉冲液体火箭发动机特性试验
13.FAILURE ANALYSIS OF THE MODEL SOLID ROCKET MOTOR CASE IN HYDROTEST某型号固体火箭发动机壳体水压破坏分析
14.Allan J.McDonald, "Design evolution of the space shuttle solid rocket motors"航天飞机固体火箭发动机的设计演变
15.Investigation of ring aerodynamic throat for solid rocket motor固体火箭发动机环缝式气动喉部研究
16.Analytical Solution of Temperature Field of Solid Rocket Motor Laminated Structure with High-Temperature Thermal Shock高温热冲击下固体火箭发动机层合结构温度场解析解
17.Reliability Design of Pressure Vessel and Its Application on Solid Rocket Motor Vessel压力容器壳体的可靠性设计及在固体火箭发动机壳体上的应用
18.Research on the Debonding Image Processing Technology for the Solid Rocket Motor with the Spinning Texture旋压壳体固体火箭发动机脱粘检测图像处理技术研究
相关短句/例句
solid ducted rocket固体火箭冲压发动机
1.Modeling and simulation on the gas generator and gas control valve ofsolid ducted rockets;固体火箭冲压发动机燃气发生器及燃气流量调节阀建模及仿真
2.Three dimension numerical simulation on air inlet ofsolid ducted rocket;固体火箭冲压发动机进气道三维数值模拟
3.Dynamic modeling and model reduction order of controllable flowsolid ducted rockets;燃气流量可控的固体火箭冲压发动机动态建模及模型降阶(英文)
3)ducted rocket motor固体火箭冲压发动机
1.There are a variety of influential factors to the combustion efficiency of secondary chamber of boron-based propellantducted rocket motor,which are difficult to be expressed accurately by analytical functions.影响含硼推进剂固体火箭冲压发动机补燃室燃烧效率的因素很多,且各因素对燃烧效率的影响很难用精确的解析函数式来表示。
4)solid ducted rocket motor固体火箭冲压发动机
1.Erosion test of the insulation in the ramjet combustor ofsolid ducted rocket motors;固体火箭冲压发动机补燃室绝热层烧蚀试验研究
2.The 3D reaction flow field in the afterburning chamber ofsolid ducted rocket motor with binary dual-underside inlet mode was numerically simulated by means of RNG κ-ε turbulence model and one step eddy-dissipation combustion model.采用RNGκ-ε湍流模型及单步涡扩散燃烧模型,对二元双下侧进气式固体火箭冲压发动机补燃室内三维反应流场进行了数值模拟,得到了补燃室二次燃烧效率的变化趋势。
3.By direct-conncted simulation calculation,the effects of common heater fuel (hydrogen,kerosene,methane and alcohol) on performance ofsolid ducted rocket motor with low-oxygen boron-based propellant were investigated.通过直连模拟计算,研究了常用加热器燃料(氢气、煤油、甲烷和酒精等)对含硼贫氧推进剂固体火箭冲压发动机性能的影响。
5)Solid liquid rocket ramjet engine固液火箭冲压发动机
6)Integral solide propellant rocket ramjet engine整体式固体火箭冲压发动机
延伸阅读
固体火箭发动机静止实验分子式：CAS号：性质：是指将装有一定质量推进剂的待测发动机，固定在地面静止试验台上进行的点火试验。静止试验主要测试压强、推力、比冲、测向分力、发动机各构件的应力、壁温和流量等参数。通过实验评定推进剂的性能以及发动机结构和性能。在火箭发动机研制、定型和生产验收等不同阶段，都要进行静止实验。
