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- To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood. 为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境,必须很好地了解稳态状态。
- It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine (LRE) monitoring system in ground test. 摘要确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。
- The dynamic models of engine parts in a new high-performance staged combustion cycle liquid propellant rocket through the module codified were built. 通过模块化编程,建立了新一代高性能补燃发动机启动过程的部件模型。
- To overcome the difficulties on acquiring enough fault modes from ground and flight test data, the failure process for liquid propellant rocket propulsion systems was modeled. 为克服由于试验或飞行数据不足而无法获取系统足够故障模式的问题,开展了液体火箭推进系统故障过程建模与计算机仿真研究工作。
- An adaptive threshold algorithm consisting of two stages based on autoregressive model was presented for monitoring the steady process of Liquid Propellant Rocket Engine(LRE) in ground test. 提出一种基于自回归模型的自适应阈值检测算法用于监测液体火箭发动机地面试验的稳态过程,该算法由两个阶段组成。
- liquid propellant rocket engine control 液体火箭发动机控制
- liquid propellant rocket projectile 液体火箭弹
- liquid propellant rocket engine test 液体火箭发动机试验
- liquid propellant rocket engines 液体推进剂火箭发动机
- reusable liquid propellant rocket engine 可重复使用液体火箭发动机
- RESEARCH ON TOXIC GAS DIFFUSION AFTER LIQUID PROPELLANT ROCKET EXPLOSION 液体火箭爆炸后有毒气体扩散研究
- liquid propellants rocket engine 液体火箭发动机
- Design and realization of primitive real-time fault detection and alarm system for liquid propellant rocket engines 液体火箭发动机实时故障检测与报警原型系统的设计与实现
- Independent Component Analysis for Fault Detection of the Liquid Propellant Rocket Engine 独立分量分析在液体火箭发动机故障检测中的应用
- Independent component analysis for the fault features of liquid propellant rocket engine 应用独立分量分析提取液体火箭发动机的故障特征
- Finite Element Analysis of the Turbine Blade Structural Characteristics for Liquid Propellant Rocket Engine 液体火箭发动机涡轮叶片结构特性的有限元分析
- Application of Wavelet Analysis in Steady Data De-nosing for Liquid Propellant Rocket Engine Test 小波分析方法在液体火箭发动机试验稳态数据去噪中的应用
- INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION TECHNOLOGY FOR LIQUID PROPELLANT ROCKET ENGINE 液体火箭发动机气动谐振点火技术的研究
- Application of evolutionary strategy of research of static characteristics of liquid propellant rocket engine 进化策略在火箭发动机静态特性研究中的应用
- Flow Analysis and Orifice Plate Design for Oxygen Chamber of a Liquid Propellant Rocket Engine 液体火箭发动机氧腔流动分析及均流板设计研究