摘要
介绍了由发动机强度设计规范及准则、强度设计软件及方法、强度设计数据库及准则库构成的航空涡喷、涡扇发动机强度设计系统。用该系统可进行发动机构件的应力、振动和寿命分析。
The turbojet and turbofan engine strength design system, which consists of the strength design specification and standard, the strength design software and method, and the strength design database, is introduced. The system can be used for the analysis of stress, vibration and life of the engine components.
出处
《航空发动机》
2003年第4期32-34,共3页
Aeroengine
