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- hypersonic ramjet 高超音速冲击式空气喷气发动机
- hypersonic ramjet engine 高超音速冲击式空气喷气发动机
- A ramjet airplane engine designed for hypersonic flight that burns fuel in the supersonic airstream produced by the plane. 超音速冲压喷气发动机:一种喷气式飞机发动机,设计用于极超音速飞行,燃料在由飞机产生的超音速气流中燃烧。
- Full-Scalc Liquid Fuel Ramjet Combustor Tests. 全尺寸液体冲压发动机燃烧室试验。
- A simple,essentially tubular jet engine,such as a ramjet. 压式喷气发动机一种简单的，主要为管道式的喷气发动机，如喷压式发动机
- In recent years the supersonic combustion ramjet (scramjet) has been undergone extensive researches.There is established a Hypersonic Propulsion Testing Facility and conducted a lot of experiments. 超燃冲压发动机是近年来航空航天方面的研究热点，国内建立的超燃实验台进行了大量的模拟实验。
- A simple, essentially tubular jet engine, such as a ramjet. 压式喷气发动机一种简单的，主要为管道式的喷气发动机，如喷压式发动机
- Ramjet: Air-breathing jet engine that operates with no major moving parts. 冲压式喷射发动机:工作时没有重要运动部件的一种喷射发动机。
- FEM FCT is used to solve three dimensional hypersonic inviscid flow. 从Euler方程出发，利用流量修正有限元法（FEM?FCT）求解三维无粘流动的高速流场。
- 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。
- Hypersonic propulsion test facility is important for the scramjet ground tests. 摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
- A conceptual design of the hypersonic civil transport is introduced here. 介绍了高超声速民用运输机的概念设计方案。
- Hypersonic wind tunnels operating at very low densities were developed starting in about 1960. 低密度超音速风洞大约开始发展于1960年。
- 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。
- Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles. 特别值得注意的是在发展超音速和高超音速飞行器的过程中，偏离了莱特理想的工作方式。
- A complete line of Horizontal Wet Process Equipment Incorporating Ramjet Technology. 结合冲压式技术，一条完整的湿流程设备水平线。
- With such a large heat sink value, FRA can meet the requirement of hypersonic flying machine. 在 80 0℃时 ,两者都具有较高的热沉值 ,分别达到 5 6 9MJ kg和 6 6 0MJ kg ,该热沉值能够满足超高音速飞行器的热管理要求。
- Air-breathing gas dynamic laser is developed as a new conception based on ramjet and gas dynamic laser. 冲压式气动激光器是在冲压发动机和气动激光器的基础上发展起来的一个新概念。
- The experimental results of low temperature ablator (beeswax and camphor) tests in the hypersonic wind Tunnel are presented in this paper. 本文给出了低温烧蚀材料的高超声速风洞烧蚀实验研究的结果。
