scramjet

Aerodynamic Performance Analysis of Scramjet Isolator under Asymmetric Supersonic Flow

非对称来流条件下超燃冲压发动机隔离段气动特性研究

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 ground test is very important for the research of scramjet.

地面实验是研制超音速燃烧冲压发动机的重要手段。

This paper summarized the latestand foreign development status of scramjet engine andthe key technologies.

超燃冲压发动机技术是一项新型的、具有广阔发展前景的推进技术.

Computational Study of Contraction Ratio Effects on Scramjet Inlet

不同收缩比超燃冲压发动机进气道的数值研究

Optimized design on a new type thermal structure of scramjet combustor

超燃冲压发动机燃烧室新型热结构的优化设计

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.