固体火箭发动机壳体,solid rocket motor vessel
1)solid rocket motor vessel固体火箭发动机壳体
1.Reliability design of CFRPsolid rocket motor vessel based on the burst experiment基于爆破试验的CFRP固体火箭发动机壳体的可靠性设计
英文短句/例句
1.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
2.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
3.Finite Element Analysis of Large Deformation and Emulation for Filament-Wound Solid Rocket Motor Case纤维缠绕固体火箭发动机壳体大变形有限元分析与仿真软件介绍
4.Establishment of Mechanical Model of High-speed and High-acceleration Solid Rocket Engine Case高速高加速固体火箭发动机壳体力学模型的建立
5.Reliability design of CFRP solid rocket motor vessel based on the burst experiment基于爆破试验的CFRP固体火箭发动机壳体的可靠性设计
6.Acousto-ultrasonic detection for interface defect between case and insulation of SRM固体火箭发动机壳体/绝热层界面缺陷的声-超声检测
7.Analysis of Failure and Optimization for Composite Case of Solid Rocket Engine固体火箭发动机复合材料壳体破坏分析及优化
8.The Development of Integral Design of Solid Rocket Motor Metal Case固体火箭发动机金属壳体综合设计技术研究
9.ANALYSIS ON DESIGN FOR HYBRID FILAMENT-WOUND CASE OF SOLID ROCKET MOTOR固体火箭发动机混杂纤维缠绕壳体设计分析
10.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
11.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
12.Analysis of dispersive characteristics of guided wave in multi-layered structure of solid rocket motor shell固体火箭发动机多层结构壳体的导波频散特性分析
13.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
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.nozzle diaphragm喷管挡栅板 -固体火箭发动机的
17.internal ballistics of solid rocket motors固体火箭发动机内弹道学
18.Research of Working Characteristic of Solid Motor in Water;固体火箭发动机水下工作特性的研究
相关短句/例句
propellant bottle固体火箭发动机外壳<火>
3)rocket engine case火箭发动机壳体
4)solid rocket motor固体火箭发动机
1.Grain design ofsolid rocket motor based on ACIS geometric modelling platform;基于ACIS几何造型平台的固体火箭发动机装药设计
2.Analysis on fluid-structural coupling ofsolid rocket motor during rapid pressurization;固体火箭发动机快速升压过程的流固耦合分析
3.Buckling analysis on rear dome ofsolid rocket motor case;固体火箭发动机壳体后封头屈曲分析(英文)
5)Solid propellant rocket motor固体火箭发动机
1.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
2.Thrust Vector Control (TVC) system of certain type solid propellant rocket motor was the research object and multibody dynamics method was adopted herein.以某型号固体火箭发动机推力向量控制系统为研究对象,采用多体系统动力学计算方法,以作用在系统活动体上的轴向载荷为工作阻力,作动器指令位移为原动件的已知运动规律,接头内引入并联非线性弹簧阻尼器表征各构件间的接触,建立该型号推力向量控制系统动力学模型,进行多体动力学计算,得到接头内构件间的实时运动规律、接触力及力矩。
3.A kind of solid propellant rocket motor is analyzed by finite element method in this paper.文中通过利用有限元分析程序对某型固体火箭发动机进行分析,初步探讨了连接结构形式和装配预紧力对发动机密封性的影响,结果表明有限元分析对于固体火箭发动机的密封性设计具有重要的指导作用。
6)Solid propellant rocket engine固体火箭发动机
1.In this paper,the temporal response of solid propellant rocket engine grain under complex overloads is analyzed.基于三维线性粘弹性积分本构关系,采用有限元法,对固体火箭发动机的药柱结构在复杂载荷作用下的瞬态响应进行了数值模拟。
2.The artificial neural networks are applied to the prediction of the specific impulse for solid propellant rocket engine.将神经网络方法引入了固体火箭发动机的比冲性能预测,该方法避开了系统具体规律分析以及相应数学模型建立所带来的困难,直接用神经网络模型来模拟真实的系统关系。
3.The temperature of a high te mperature, high pressure plume solid propellant rocket engine is difficult to me asure but is useful for determining the combustion status of the engine.对于固体火箭发动机羽焰温度的测量是困难的,了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。
延伸阅读
固体火箭发动机见导弹推进系统。
