Scramjet nozzle was installed at the exit of the combustor.

尾喷管直接安装在模型发动机的燃烧室出口。

The scramjet is composed of inlet, isolator, combustor and nozzle.

超燃冲压发动机由进气道、隔离段、燃烧室和尾喷管组成。

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.

It achieves hypersonic speed using a special sort of engine known as a scramjet.

它通过一种叫做超音速燃烧冲压式喷气发动机的特殊发动机来实现超音速。

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows.

本文通过数值模拟得到了超燃冲压发动机燃烧室化学反应流流场的流动结构.

Preliminary investigation for scramjet engine performed by Beijing Power Machineries Institute is described in this paper.

介绍了北京动力机械研究所进行的超燃冲压发动机初步研究.

Advanced ramjet technologies are also important for scramjet development, and the Chinese have been active in this area for decades.

先进亚燃冲压技术对于超燃冲压技术至关重要，而中国数十年来在这一领域一直很活跃。

Both NASA and DARPA have been dabbling in scramjet technology for years, creating a vast body of knowledge and data for engineers to build upon.

美国太空署与国防部高级研究计划局数年来已经在超燃冲压发动机技术上倾注气力，为工程师创造了可信赖的广大知识体系和数据。

Chinese engineers from several research facilities presented about a dozen papers on their scramjet developments, as well as details on the new wind tunnel.

来自几家研究机构的中国工程师发表了十多篇关于冲压技术的发展和新风洞细节的论文。

Due to extremely short residence time of supersonic airflow, it is difficult to effectively mix and combust for the fuel and air in scramjet combustor.

高超声速气流在燃烧室的停留时间非常短，使得超燃冲压发动机燃烧室内燃料与气流的混合及其燃烧变得非常困难。