as an example, the development of a high bypass ratio turbofan engine was used to demonstrate how the constraints restrict design cycle parameters.
以发展大涵道比涡扇发动机为例,说明了约束条件对设计循环参数的限制。
modern low bypass ratio turbofan engine is the heart of the new fighter, whose performance and aerodynamic stability greatly affect the characteristics of the new fighter.
涡扇发动机作为现代战斗机的心脏,其性能和稳定性对战斗机的性能和稳定性能有很大的影响。
the case study of a high bypass ratio turbofan engine has verified the feasibility of a three-layer back propagation network.
通过一个高涵道比涡扇发动机故障诊断的实例分析,验证了三层逆传播网络的可行性。