rocket engine的例句大全

Effect of aspect ratio on heat transfer and fluid flow in regenerative cooling channel of liquid rocket engine thrust chamber

通道深宽比对液体火箭发动机推力室再生冷却的影响

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Application of PCA in Sensor Fault Diagnosis of Rocket Engine Ground Testing Bed

PCA在火箭发动机试车台传感器故障诊断中的应用

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Through two methods measuring cutoff thrust and pressure of com-bustion chamber when testing liquid propellant rocket engine on ground, cu-toff impulse as simulated altitude condition is obtained. These methods are revie-wed simply, too.

本文叙述在地面条件下试验液体火箭发动机时，通过测量发动机后效段推力与测量发动机燃烧室压力两种方法来求得模拟高空后效冲量，并对这两种方法作简单评论。

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Fault diagnosis of rocket engine ground testing bed based on KPCA and SVM

基于KPCA和SVM的火箭发动机试验台故障诊断方法

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Finally, the applicability and effectiveness of the proposed methodology is illustrated by some sensors in the rocket engine ground testing bed liquid hydrogen providing system.

最后，以液体火箭发动机试车台氢供应系统几个关键传感器的故障诊断为例验证了这种方法实用性和有效性。

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The theoretical specific impulse formula for two-phase flow in nozzle of rocket-ramjet engine is derived on the basis of similarity to that used for rocket engine.

本文导出了类似于火箭发动机的火箭冲压发动机喷管的两相流动理论比冲公式；

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Numerical Analysis and Application of Wall Temperature History for Liquid Rocket Engine Thrust chamber with Radiation Cooling

液体火箭发动机辐射冷却推力室壁温响应的数值分析及应用

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The Analysis of Test Failure of Solid Rocket Engine

固体火箭发动机试验故障分析

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Rocket engine test stand exerts force on a load cell.

火箭发动机试验的立场，施加武力对负载细胞。

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Review of combustion instability testing research on liquid propellant rocket engine

液体火箭发动机燃烧不稳定性试验研究简述

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The two phase turbulent combustion steady process and high combustion instability in the liquid rocket engine are simulated with the method of computational combustion dynamics.

采用计算燃烧学的方法对发动机燃烧室内的湍流两相燃烧过程的稳定燃烧状态和高频不稳定燃烧现象进行了数值模拟。

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Constant Temperature Remote Control System for Solid Rocket Engine Pushing Core Model

固体火箭发动机插芯恒温远程控制系统

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Measurement technology of thermocouple sensor in the liquid rocket engine test

液体火箭发动机试验热电偶传感器测量工艺

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Automatic calibration of rocket engine thrust measurement at the testing location

火箭发动机推力测量的原位自动校准

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Grain design for hybrid rocket engine with cluster type thrust chamber

带簇式推力室的固液火箭发动机装药设计

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The Effect of Heat Shield on Temperature Distribution of Rocket Engine Thrust Chamber

隔热罩对火箭发动机推力室温度场的影响

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Experimental research on the thrust chamber of tripropellant rocket engine

三组元火箭发动机推力室试验研究

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Numerical Simulation of Chemical Reacting Flow in H 2/ O 2 Rocket Engine Thrust Chamber

氢氧发动机推力室化学反应流场计算

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Research of damage mitigating control of thrust chamber based on fuzzy logic reasoning for liquid propellant rocket engine

基于模糊推理的液体火箭发动机推力室减损控制研究

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A sample of rocket engine thrust chamber with cooling channels was successfully manufactured by APEF.

成功制造出带冷却通道的火箭发动机推力室身部样件。

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