2) motor optimization design
发动机优化设计
3) aero-engine design
航空发动机设计
1.
In order to overcome the difficulties in advanced aero-engine design, such as complex coupling relations and serious conflicts between different disciplines, the research, development and application of key technologies of MDO have been carried out in three phases: part design, component design and whole engine preliminary design.
针对先进航空发动机设计面临的各学科间耦合关系复杂、指标冲突严重等困难,按零件、部件和总体方案设计3个阶段对MDO的各项关键技术开展了研究、开发及应用工作,提出了基于MDO技术的航空发动机一体化设计方法。
6) optimal designs/special type engine
最优设计/特种发动机
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