scramjet nozzle
基本解释
- [航空、航天科学技术]超燃冲压发动机尾喷管
英汉例句
- 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。 - In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.
最后，本文针对两种构型的超音速尾喷管，对其流场进行了计算和分析。 - 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。
双语例句
专业释义
- 超燃冲压发动机尾喷管