propellant combustion的例句大全

In MPT system, the microwave resonator is the important component, which is in charge of the gas propellant's absorbing and transforming the microwave energy, just like the combustion chamber in chemical propulsion.

在MPT中，微波谐振腔是工质吸收与转换微波能量的重要场所，它的功能和化学推进的燃烧室一样。

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It is considered that the combustion surface and the heat feedback of the propellant are increased by addition of ACP, leading that the increasing of burning rate of the propellant.

分析了ACP提高无烟改性双基推进剂燃速的作用机理，认为ACP可增加燃烧表面积和热量向燃烧表面积的反馈，使推进剂的燃速大增。

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This paper presents computation and analysis of tangential mode of high frequency combustion instability in FY-20 liquid propellant rocket engine by means of the annular instability model.

本文用环形不稳定性计算模型计算、分析了FY-20液体火箭发动机的切向高频燃烧不稳定性。

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the radial acceleration forces can cause greater retention of the solid phase combustion products near the propellant surface.

径向加速度的力量可以造成更大的保留固相燃烧产物附近的推进剂表面。

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effects of physical dimension on combustion performance of tubular variable-burning-rate gun propellant

几何尺寸对管状变燃速发射药燃烧性能的影响

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in this paper, a new parameter named slurry combustion effect was induced for applying solid propellant bdp model for prediction of pasty propellant and slurry propellant steady combustion behavior.

在固体推进剂BDP燃烧模型基础上，引入膏体推进剂燃烧热效应这一新参数将模型推广于膏体推进剂和固体推进剂药浆燃烧研究。

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effect of azide nitrate ester on combustion behaviour of nitramine modified double base propellant

叠氮硝酸酯对硝胺改性双基推进剂燃烧性能的影响

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exploring suppression of oscillating combustion of hap tri-component propellant in revolving combustion chamber

HAP三组元燃料旋转燃烧室振荡燃烧外部激励研究

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detection study on the start process for liquid propellant rocket engine with staged combustion cycle

液体火箭发动机启动过程检测研究

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propagating process of cracks on polysulfide propellant during combustion

聚硫推进剂燃烧条件下裂纹扩展过程的研究

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the effect of acp on the energy and combustion performance of smokeless modified double-base propellant

ACP对无烟改性双基推进剂能量和燃烧性能的影响

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influences of lead salts on combustion characteristics of high energy smokeless modified double-base propellant

铅盐对高能无烟改性双基推进剂燃烧性能的影响

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effect of grain size on progressive combustion of the variable burning rate propellant

药型尺寸对变燃速发射药燃烧渐增性的影响

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Nevertheless , particle size distribute does not change with the combustion chamber pressure and propellant powder percentage.

粒子尺寸分布不随燃烧室压强和推进剂铝粉含量变化.

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Aim To study the actual combustion law of deterred propellant charge in bore.

研究钝感火药装药膛内的实际燃烧规律.

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This paper introduces theoretical formulation optimization and ignition and combustion experiments of liquid propellant.

文内简述了液体药理论配方优选和液体药点火、燃烧实验研究.

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The ignition and combustion characteristics of pasty propellant are important parameters for the motor design.

膏体推进剂的点火和燃烧特性是发动机设计的重要参数.

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Influence of some straight chain azido-nitramine on combustion properties of CMDB propellant

直链叠氮硝胺对双基推进剂燃烧性能的影响

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The atomization mechanism of hypergolic rocket propellant and decomposition combustion at high pressure and turbulence burning of premixed reactant flow field are considered.

数值仿真模型中考虑了自燃推进剂雾化机理、高压分解燃烧和预混反应流湍流燃烧等。

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Thermal Decomposition Mechanism, Non-isothermal Reaction Kinetics of Bismuth Citrate and Its Catalytic Effect on Combustion of Double-base Propellant

柠檬酸铋的热分解机理、非等温反应动力学及其对双基推进剂燃烧的催化作用

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