为了使军用发动机系统的性能更优良，设计效率更高，本文对某军用发动机主要零部件组合结构进行了动态特性的研究。
In order to enhance the performance and design efficiency of military engine system, dynamic features of combined structure of military engine main parts are researched.
进口流场的温度畸变对军用飞机发动机稳定性具有比压力畸变更大的影响。
Temperature distortion on inlet flow of engine is more important than pressure distortion for engine stability.
军用直升机使用西方发动机并不是新闻。
This use of Western engines in military helicopters is not new.
应用推荐