scramjet

英 美

网络  超燃冲压发动机; 超音速燃烧冲压发动机; 超音速冲压式喷气发动机; 超音速冲压喷射装置; 冲压发动机

COCA.37556

双语例句

  1. The results show that the strut-rocket scramjet can provide robust ignition and combustion efficiency and wide operability for ambient liquid hydrocarbon fuel in large scale combustor.
    利用支板火箭与轴对称圆形燃烧室相结合能在较短燃烧室内实现高效燃烧，为将来开展大尺寸超燃冲压发动机燃烧技术研究奠定基础。
  2. The research coinstantaneous shows that the boundary transition should be considered, and effective transition method should be adopted to ensure the normal work of the scramjet engine.
    同时说明，在超燃进气道设计过程中，需要充分考虑边界层转捩问题，引入有效的边界层转捩控制方法，以保证发动机的正常工作。
  3. Catalytic reforming gas generator is the effective method of producing on-line hydrogen, which is good for the ignition and combustion of hydrocarbon fuel in the scramjet.
    催化重整燃气发生器是在线产生氢气的有效途径，有助于碳氢燃料超燃冲压发动机的着火和燃烧。
  4. Research on Numerical Simulation of Two-Phase Reacting Flow Field and Combustion Performance of Annular Combustors; Simulation and Experiment of Two-Phase Mixing and Combustion in the Scramjet Combustor
    环形燃烧室两相燃烧流场与燃烧性能数值研究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
  5. Influence of Back Pressure on the Inner Flow Field in Scramjet Isolator
    反压对超燃冲压发动机隔离段内流场的影响
  6. Research on Numerical Simulation for Integrated Flow Field of Supersonic Inlet and Combustor; Simulation and Experiment of Two-Phase Mixing and Combustion in the Scramjet Combustor
    弹用超声速进气道/补燃室流场及其一体化数值模拟研究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
  7. 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。
  8. The facility is to provide high enthalpy [ thermal dynamic] model scramjet testing, he says.
    该实验室将提供高焓值[热动力学]模型超燃冲压发动机测试，他说。
  9. A Investigation of on Chip Parasitic Parameter Extration; Three-dimensional Massively Parallel Numerical Simulation of Kerosene-fueled Scramjet
    超大规模集成电路寄生参数提取研究煤油超燃冲压发动机三维大规模并行数值模拟
  10. Catastrophe Characteristics of Mode Transition in Scramjet
    超燃冲压发动机模态转换突变特性研究
  11. Wind tunnel experiment of the influence of dynamic change of attack angle on start property of sidewall compression scramjet inlet
    攻角动态变化对侧压式进气道起动特性影响的风洞试验
  12. Parametric sensitivity analysis of scramjet nozzle configuration
    超燃冲压发动机尾喷管构型参数灵敏度分析
  13. Configuration Effect Analysis of Scramjet Combustor Based on the Integral Balanceable Method
    基于综合平衡法的超燃冲压发动机燃烧室构型影响分析
  14. Numerical simulation of three dimension viscous flow of combustion-heater used for scramjet test
    超燃试验用加热器三维粘性流场数值模拟
  15. The drag of cavity decreases with increasing fuel equivalence ratio, and could be converted into the thrust, instead of drag, under combustion mode which is close to real statue of scramjet.
    在实际超燃冲压发动机工况下，凹腔火焰稳定器的阻力随着当量比的增加而减小，并最终会表现为正推力。
  16. Computation and analysis of aeroheating of scramjet inlet cowl lip
    超燃冲压发动机唇口气动热计算研究与分析
  17. The Influence of Dual-cavity on Pilot Hydrogen Distribution in Scramjet Combustor
    超燃冲压发动机燃烧室中双凹腔对引导氢分布的影响
  18. 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
  19. Investigation on drag of cavity flame holder in scramjet Simulation of turbulent lean premixed flame in aircraft engine
    超燃冲压发动机凹腔火焰稳定器阻力分析贫燃料湍流预混燃烧火焰稳定性的数值研究
  20. The uniform design and response surface methodology ( RSM) are applied to the multi-objective optimization of a2-D mixed compression scramjet inlet.
    基于响应面法进行了二维混合压缩超燃冲压发动机进气道的多目标优化研究。
  21. 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
  22. A scramjet engine goes as fast as a rocket, but it doesn, t have to carry its own oxygen supply.
    超音速燃烧冲压式喷气发动机能使飞行像火箭一样快，但它不必自携氧气。
  23. 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。
  24. The thermal environment of the scramjet strut leading edge is rigorous.
    在超燃冲压发动机工作过程中，支板前缘的热环境非常恶劣。
  25. 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
  26. Three-dimensional Massively Parallel Numerical Simulation of Kerosene-fueled Scramjet
    煤油超燃冲压发动机三维大规模并行数值模拟
  27. Effects of non-equilibrium chemical reaction flow on the performance of scramjet nozzle
    化学非平衡流动对超燃冲压发动机尾喷管性能的影响
  28. Simulation on In-Cylinder Flow on Mixture Formation and Combustion in OPOC Engine Experimental study on the combustion and flow process in a scramjet with strut injector
    对置二冲程柴油机缸内流动形式对混合气形成及燃烧的模拟研究超燃冲压发动机支板喷射燃料的燃烧过程试验
  29. Feasibility study of MHD energy bypass scramjet
    MHD能量旁路超燃冲压发动机可行性分析
  30. Investigation of the effect and optimization of heat release distributions in the combustor on scramjet performance
    释热分布对超燃冲压发动机性能的影响及优化
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