根据航空发动机结构完整性大纲，对于断裂关键件必须进行损伤容限设计分析。
According to aeroengine structure integrity program, fracture critical components must be analysed with damage tolerance concept.
根据航空发动机结构完整性大纲，对于断裂关键件必须进行损伤容限设计分析。
According to aeroengine structure integrity program, fracture critical components must be analysed with damage tolerance concept.
应用推荐