1) 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。
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) Multi mode ramjet
多模态冲压发动机
4) dual-fuel scramjet
双燃料超燃冲压发动机
1.
A simple performance analysis model for dual-fuel scramjet is proposed to evaluate the fuel selection effect on vehicle performance,as range selected as mission performance measure.
提出了双燃料超燃冲压发动机方案,以航程为高超声速巡航飞行器性能目标,建立了双燃料超燃冲压发动机的性能分析模型,得到了超燃冲压发动机燃料类型的选择准则。
5) 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。
6) 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
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。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条