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1)  Multi mode ramjet
多模态冲压发动机
2)  dual-mode scramjet
双模态超燃冲压发动机
1.
Experiment and Numerical Simulation Investigation of Dual-Mode Scramjet;
双模态超燃冲压发动机试验与数值仿真研究
3)  dual-mode scramjet
双模态冲压发动机
1.
On the basis of direct-connect scramjet test system simulating flight Mach number 4,different injection modes were compared to study the influence of flame stability on fixed geometry dual-mode scramjet combustor fueled with liquid kerosene and ignited with torch-model ignition.
在模拟飞行马赫数Ma=4的直连式试验设备基础上,采用固定几何双模态冲压发动机燃烧室构型,使用液体煤油作为燃料,并用火炬式点火器点火,研究不同喷注方式下的火焰稳定性。
4)  scramjet model
超燃冲压模型发动机
1.
Research on the ignition and combustion performance of kerosene in a direct-connected scramjet model was conducted.
46的大范围内,煤油在超燃冲压模型发动机中能够成功点火,支板和凹腔对煤油在超声速气流中的点火及稳定燃烧有重要作用,少量氢气的喷入对煤油的点火燃烧有良好的促进作用。
5)  ramjet [英]['ræmdʒet]  [美]['ræmdʒɛt]
冲压发动机
1.
Investigation on a thrust vector design scheme of ramjet;
一种冲压发动机推力矢量设计方案研究
2.
Improved BP Neural Network and its Application in Performance Predicting of Ramjet;
改进BP神经网络在冲压发动机性能预测中的应用
3.
A simplified method to analyze injecting phenomena and its application to ramjet combustion chamber;
冲压发动机燃烧室燃料喷射的简化计算方法研究
6)  ramjet engine
冲压发动机
1.
Design method of regulating rule for ramjet engines based on similarity parameters;
基于相似参数的冲压发动机调节规律设计方法(英文)
2.
Analysis of the powdered carbon combustibility in secondary combustion chamber for rocket ramjet engine;
碳粉燃料在火箭冲压发动机补燃室内燃烧特性的分析
3.
Numerical simulation of the ramjet engine separation flow;
冲压发动机转级流场数值仿真研究
补充资料:航空发动机推重比(见航空发动机推力)


航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine

  hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
  
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