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- A simulation model of liquid fuel ramjet engine for missile was developed. 发展了一种弹用液体冲压发动机仿真模型。
- Digital electronic control system of a liquid fuel ramjet engine 液体冲压发动机数字电子控制系统换
- Full-Scalc Liquid Fuel Ramjet Combustor Tests. 全尺寸液体冲压发动机燃烧室试验。
- Liquid fuel ramjet engine 液体冲压发动机
- liquid fuel ramjet (LFRJ) 液体冲压发动机
- Liquid fuel ramjet 液体冲压发动机
- ZHANG Wei,ZHU Hui,FANG Ding-you,et al.Fuel-rich propellant fuel mass flow solid for adjustable ramjet engine[J].Journal of Propulsion Technology,1999,20(5):95-98. [5]张炜;朱慧;方丁酉;等.;用于燃气流量可调固冲发动机的富燃推进剂[J]
- Green liquid fuel stove for alcohol. 液体绿色燃料用于酒精炉。
- Supersonic combustion ramjet engine is a new type of jet engine, the combustion of the fuel used high-speed flight generated by the compressed air, can be obtained directly from the oxygen in the air. 超音速燃烧冲压式喷气发动机是一种新型发动机，其燃料的燃烧利用了高速飞行所产生的压缩气流，能直接从空气中获取氧气。
- The internal combustion engine is most common: this obtains its power by burning a liquid fuel inside the engine cylinder. 内燃机是最常见的：它通过在发动机汽缸里面燃烧一种液体燃料获得动力。
- The rockets give the planes and missiles enoughspeed to make the ramjet engine workable. 这种助推火箭为飞机和导弹提供足够的速度，以使冲压式喷气发动机可以开动工作。
- The rockets give the planes and missiles enough speed to make the ramjet engine workable. 这种助推火箭为飞机和导弹提供足够的速度,以使冲压式喷气发动机可以开动工作。
- In this paper, fistly, the combustion and flow in solid fuel ramjet are analyzed, the physical model of the double-cone inlet and combustor within SFRJ are established. 本文首先分析了固体燃料冲压发动机内的流动和燃烧现象，采用双锥型扩压器的进气道和燃烧室模型；
- In order to verify the ignition and combustion performances of the metal-powder fuel ramjet,preliminary direct-connected test for the motor was carried out. 为了检验金属粉末燃料冲压发动机的点火及燃烧特性,对设计的发动机进行了初步的直连式试验研究。
- Liquid fuels also burn only when the surface of the liquid is in contact with air. 液体燃料也只有当液体表面与空气接触时才会燃烧。
- Breathing can be divided into jet engine turbojet engine, turbo-fan jet engine and combustion ramjet engine. 如果按照这一定义，除远程巡航导弹外，各种飞航式反舰导弹和空地、空舰飞航式导弹也属于巡航导弹。
- In this paper, fistly, the combustion and flow in solid fuel ramjet are analyzed, the physical model of the inlet and combustor within SFRJ are established. 本文首先分析了固体燃料冲压发动机内的流动和燃烧现象，建立了SFRJ的进气道和燃烧室模型；
- Ramjet engine is ideal propulsive equipment for new supersonic missile, and supersonic inlets are important components. 冲压发动机是新一代超声速导弹理想的动力装置,超声速空气进气道是它的一个重要部件。
- A liquid fuel which easily evaporates and turns into vapour is called "volatile". 易于蒸发和变成气体的液体燃料叫作“挥发性”燃料。
- The ramjet engine has many advantages such as simple structure, light weight, little volume, big ratio of pushing and gravity, low cost, and etc. 冲压发动机具有结构简单、重量轻、体积小、推重比大、成本低等一系列优点。
