SCRJ:超音速燃烧冲压发动机
“超音速燃烧冲压发动机”的英文全称为Supersonic Combustion RamJet,其常用缩写SCRJ便于快速书写和使用。这一专业术语多见于航空航天领域的文献与报告中,尤其在美国国家航空航天局的相关技术资料中频繁出现。这种发动机技术是高超音速飞行器的关键动力装置,通过超音速气流中的燃烧过程实现高效推进,代表了航空航天推进系统的前沿发展方向。
Supersonic Combustion RamJet具体释义
Supersonic Combustion RamJet的英文发音
例句
- The necessity about using supersonic combustion ramjet ( scramjet ) for the single stage to orb (?) t aerospace plane is demonstrated.
- 本文首先说明了单级入轨的空天飞机采用超声速燃烧冲压发动机的必要性。
- The internal flow fields of supersonic combustion ramjet ( scramjet ) combustion chamber with strut or normal wall injectors are simulated numerically by using the Favre-averaged Navier-Stokes equations with the Baldwin-Lomax algebraic turbulence model.
- 应用含组分守恒方程的质量平均Navierstokes方程和BL代数湍流模型,数值模拟了后台阶构型燃烧室在采用台阶上游支板引射和壁面垂直引射燃料时的内部流场。
- Numerical Simulation on Supersonic Combustion of Fuel-rich Gas for a Dual Combustor Ramjet Simulation and Experiment of Two-Phase Mixing and Combustion in the Scramjet Combustor
- 双燃烧室冲压发动机富油燃气超声速燃烧数值模拟超燃冲压发动机燃烧室两相流混合燃烧过程仿真及实验研究
- Analysis of the hydrogen combustion field in scramjet dual-cavity combustor Numerical Simulation on Supersonic Combustion of Fuel-rich Gas for a Dual Combustor Ramjet
- 超燃冲压发动机双凹腔燃烧室氢气燃烧流场分析双燃烧室冲压发动机富油燃气超声速燃烧数值模拟
- Investigation on supersonic combustion of fuel-rich hot gas as reacting jets in ramjet / scramjet combustor
- 双燃式冲压发动机中富油燃气射流的超燃研究
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