潜射导弹

潜射导弹尾部燃气后效建模及数值模拟

The Model of Combustion Gas Bubble of Submarine-launched Missile and Numerical Simulation

均匀设计法在潜射导弹出水试验中的应用

The Application of Unifom Design Method to Exiting Water Test for Submarine-launched Missile

本文建立了潜射导弹水下发射的内流场数学模型，采用有限体积法（FVM）对无动力导弹潜艇发射时的内流场进行了模拟计算。

Simulation of the interior flow of submarine-based powerless missile underwater launching is performed by applying the finite volume method .

潜射导弹遥测系统射前快速检测技术

Quick Test Technic for Telemetry System at Missile Prelaunch Checkout Under Water

潜射导弹运动特性分析与测试

Analysis and Testing on Dynamic Characteristics of Submarine Launched Missile

潜射导弹水下动载荷识别仿真分析

Simulation Identification of Dynamic Load of Submarine - launched Missile

潜射导弹水下垂直自抛发射过程研究

Research on the vertical launching of direct igniting underwater missile

潜射导弹筒盖系统弹性缓冲支撑方案研究

Study of Flexible Supporting Schemes of Launcher Cover System for Submarine-board Missile

潜射导弹发射原点测量方法

Measurement of Launch Point of Submarine - launched Missile

价值工程在提高潜射导弹武器系统可用性中的应用

The Application of Value Engineering for Improving the Availability of Submarine Launched Missile System

潜射导弹运载器分离体下沉弹道散布影响因素仿真分析

Simulation and Analysis of the Distribution of Submarine - launched Missile Carrier Sinkage Trajectory

潜射导弹垂直发射过程空化特性研究

Research on cavitation of vertical launch submarine missile

潜射导弹的空化特性研究

Research on Cavitation for Under-water Launching Missile

潜射导弹运载器水弹道动力系统建模及其应用研究

Theory and Application Study on Underwater Trajectory Dynamic System Modeling of Submarine Launched Missile Carrier

潜射导弹运载器分离体砸艇概率仿真建模

Modeling and Simulation of the Probability of Submarine - Launched Missile Carrier Smashing the Submarine

潜射导弹运载器的艇体扰流场计算

Calculation on Submarine Perturbing Flow field of a Missile Carrier Launched by a Moving Submarine

潜射导弹水下发射及出水过程三维数值研究

3D Numerical Simulation on the Process of the Missile Underwater Launching and Exiting from Water

基于遗传算法进化神经网络的潜射导弹筒盖压力预测

Pressure Forecasting of Submarine-Borne Missile Cover System Based on Neural Network Evolved by Genetic Algorithm

轴向载荷对潜射导弹横向振动特性影响分析

Analysis of Effect of Axial Load on Lateral Vibration of Underwater - to - Surface Missile

本文主要研究分析了潜射导弹垂直出水过程中载荷特性和出水姿态的变化。

The paper mainly studies water-exiting load of the submarine-based missile and the changes of attitude .

在考虑了海流及波浪影响的情况下，建立了基于Matlab/Simulink的潜射导弹运载器下沉过程的动力学模型；

The Matlab / Simulink model of the sinking process was established considering the ocean current and wave .

研究了潜射导弹水下垂直自抛发射过程中的复杂多相流动问题。

Research is conducted on the complex multiphase flow of the vertical launching of a direct igniting underwater missile .

在分析了潜射导弹充气均压系统结构的基础上，建立了完整的充气均压系统数学模型。

Based on analysis of pressure servo system used in under-water launched missile , the complete mathematical model was established .

本文对我国某型号潜射导弹，研究了导弹在空气中受到中高频激励时的动力学响应。

This article has done some research on the dynamic response when the Chinese submarine-launched missile get a intermediate frequency excitation .

潜射导弹垂直发射出水动响应数值模拟导弹水下动机座垂直发射过程的水动力计算

The Numerical Simulation of Water-Exit Dynamic Response of Submarine Vertical-Launched Missile The hydrodynamic computation on moving base vertical launching of underwater missile

分析了容错控制技术在潜射导弹中的重要作用，指出了容错控制技术在潜射导弹中的应用方向。

The separation of guidance instrumentation systematic error ( GISE ) plays a vital role in the submarine launched missile precision analysis .

在小型水槽中，利用缩比模型和高速空气射流模拟潜射导弹水下点火喷气推进装置的工作环境，进行了喷流诱导脉动压力场的实验研究。

To simulate the operation environments for propulsion systems of subsurface missiles , a small glass-sided water flume was used for the experiments .

出水过程是潜射导弹能否成功发射的关键，各国均有因出水过程的干扰而导致发射失败的先例。

As the crux of this technology , water-exit course which involves in two-phase boundary used to result in precedent failure in certain countries .

为了有效地、多快好省地解决潜射导弹运载器上述的关键技术问题，需要在多次实航试验中，反复试验，对控制参数不断调整才能达到预期效果。

In order to solve the above key technologic problems , adjusting controlling parameters time after time in practical navigation experiments to reach expected result is needed .

此外美国空军正在成功试验的多弹头分导重返大气层运载工具可以大大加强洲际导弹和潜射导弹的破坏力。

The U.S. Air Force was successfully testing Multiple Independently Targetable Reentry Vehicles [ MIRVs ] that would significantly augment the destructive capability of ICBMs and SLBMs .