2) engine characteristic computing
发动机特性计算
1.
Based on the analysis and design of objectedoriented, the simulation model of engine characteristic computing was defined three levels: component computing, fluid computing, and flowrelation computing The three levels were summarized as a classarrangement model The extensity and reforming of the modeling is showed with an example of turbofan characteristic computin
基于面向对象分析与设计的思想 ,将发动机特性计算的仿真模型概括为部件、工质流、流动关系 3个层次 ,并将这种层次关系表达为类属层次结构。
2.
In jet engine characteristic computing,Back-Propagation network model was established to study and identify the data of engine component characteristics.
在发动机特性计算中,建立了BP神经网络对部件特性数据进行识别学习,实现了特性数据的精确插值和对未知特性数据的推测。
5) engine performance
发动机性能
1.
The engine performance LabVIEW virtual instrument test system design and implementation;
发动机性能虚拟仪器测试系统设计
2.
Influence of Combustion Chamber Geometry on In-cylinder Flow Field and Engine Performance;
燃烧室几何形状对缸内气体流动和发动机性能的影响
3.
Multi-object optimization design for improving the engine performance;
提高发动机性能的多目标优化设计
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