A dual-mode scramjet model engine with a rear-faced step is experimentally investigated with different hydrogen fuel injection manners.
在一个有突扩台阶的氢燃料高超声速冲压发动机模型内研究了氢燃料喷注方式对点火与燃烧效果的影响。
Scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.
采用遗传算法对某试验超燃冲压模型发动机的燃烧室构型参数进行了优化设计，所得方案的性能大大优于实际方案。
Furthermore, the brake system model, drive system model, engine system model and dynamics equations of whole vehicle are combined to finish the design of the substrate system.
结合汽车制动系统、传动系统和发动机系统及整车动力学四大模型，完成了下层子系统的设计。
Based on the analysis of EMS (Energy management System) engineering, a CIM (Common Information Model) engine-based dynamic interface generation and management technique is put forward.
分析了能量管理系统(ems)的工程化特点，提出了一种基于公共信息模型(CIM)引擎的动态界面生成管理技术。
Based on the analysis of EMS (Energy management System) engineering, a CIM (Common Information Model) engine-based dynamic interface generation and management technique is put forward.
分析了能量管理系统(ems)的工程化特点，提出了一种基于公共信息模型(CIM)引擎的动态界面生成管理技术。
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